Hydrodynamic Limit of the Boltzmann Equation toward Generic Riemann Solutions with Shocks
May 23, 2026
We establish the hydrodynamic limit of the one-dimensional Boltzmann equation with hard-sphere collisions toward Riemann solutions of the compressible Euler system. The Riemann solutions covered by our result include generic superpositions of elementary waves: either two shock waves and a contact discontinuity, or a rarefaction wave, a contact discontinuity, and a shock wave. For suitably well-prepared initial data and sufficiently small wave strength, we prove that the corresponding Boltzmann solution exists globally in time and converges, as the Knudsen number vanishes, to the local Maxwellian associated with the Riemann solution in \(L^2([0,T]\times\mathbb{R}_x\times\mathbb{R}^3_\xi)\) for any \(T>0\). The shock locations are modulated by dynamical unknowns, the Shifts, which are obtained as BV functions on \([0,T]\). A distinctive point of our result is that the convergence is proved without removing either the shock layer or the initial layer. In the special case of a single shock, our analysis gives a sharp quantitative description of the kinetic shock layer, up to the dynamically selected Shift. The proof combines the macro-micro decomposition, a kinetic adaptation of the \(a\)-contraction method for shocks, layer analysis, and compactness arguments for the Shifts.
The derivation of fluid equations from kinetic theory is one of the classical problems originating in the works of Maxwell and Boltzmann and in Hilbert’s sixth problem. In the kinetic description of a rarefied gas, the state of the gas is described by a distribution function \(f(t,x,\xi)\), depending on position and molecular velocity. By contrast, the macroscopic equations of fluid mechanics involve only finitely many fields, such as density, momentum, and temperature. Thus the passage from kinetic theory to fluid dynamics is, at its core, a closure problem: the Boltzmann equation contains an infinite hierarchy of velocity moments, whereas the fluid equations retain only the moments associated with the collision invariants.
The small parameter governing this passage is the Knudsen number \[\kappa=\frac{\lambda_{\mathrm{mfp}}}{L},\] the ratio between the molecular mean free path \(\lambda_{\mathrm{mfp}}\) and the macroscopic length scale \(L\). In the regime \(\kappa\ll1\), collisions occur on a much shorter scale than the macroscopic variation of the gas. The collision operator is therefore dominant, and the distribution is expected to relax rapidly toward a local Maxwellian. Since local Maxwellians are parametrized only by density, velocity, and temperature, this relaxation provides the formal closure mechanism leading to the compressible Euler equations.
The smooth compressible Euler limit of the Boltzmann equation has a long history. Nishida obtained an early analytic result [1] which may be viewed as a rigorous realization of the Maxwellian closure mechanism. Indeed, multiplying the Boltzmann equation by the collision invariants gives exact balance laws for mass, momentum, and energy. These balance laws are not closed in general, because the stress tensor and the heat flux involve higher velocity moments of the distribution function. If, however, the distribution is a local Maxwellian, the non-equilibrium stress and heat flux vanish, and the macroscopic balances close to the compressible Euler system. Nishida justified this closure in the zero-mean-free-path limit for small analytic perturbations of an absolute Maxwellian, using the spectral theory of the linearized Boltzmann equation and an abstract Cauchy–Kowalewski theorem in a scale of analytic Banach spaces.
It is useful to distinguish this moment-closure viewpoint from the asymptotic-expansion viewpoint. In the former, the main issue is to prove that the kinetic solution is confined near the local Maxwellian manifold and that the higher-moment closure defects vanish in the limit. In the latter, one seeks an order-by-order representation \[F^\kappa = M[U] + \kappa F_1 + \kappa^2 F_2 +\cdots,\] where the leading term \(M[U]\) is a local Maxwellian and the higher-order terms are obtained by solving linearized collision equations subject to solvability conditions. Hilbert and Chapman–Enskog expansions give detailed higher-order information, including Navier–Stokes corrections, initial layers, boundary layers, and shock-layer corrections. At the same time, such expansions are tied to the regularity of the leading macroscopic profile and become delicate, or break down, when the limiting Euler solution develops discontinuities.
Caflisch [2] and Ukai–Asano [3] developed Hilbert-expansion approaches to the smooth compressible Euler limit, including the treatment of initial layers. More recent works refined these arguments in \(L^2\)-\(L^\infty\) frameworks, notably the work of Guo–Jang–Jiang [4], which revisited Caflisch’s compressible Euler limit and proved the validity of the Hilbert expansion before shock formation.
These smooth-limit results justify the kinetic-to-fluid transition only as long as the limiting Euler flow remains smooth. In this sense, they describe the pre-shock classical regime of compressible gas dynamics. The restriction is not merely technical; it reflects the structure of the known methods. The usual expansion and stability arguments are organized around a smooth local Maxwellian field and require uniform control of the macroscopic derivatives. When shocks form, the limiting Maxwellian becomes discontinuous, higher-gradient corrections and kinetic layers enter the asymptotics, and the smooth-limit framework no longer applies directly.
A notable contrast is provided by the Euler–Poisson setting. Guo–Jang [5] obtained a global Hilbert expansion for the Vlasov–Poisson–Boltzmann system toward the compressible Euler–Poisson system, precisely because the limiting Euler–Poisson flow remains globally smooth. The self-consistent electric field suppresses shock formation for small irrotational perturbations through the dispersive Klein–Gordon effect first exploited by Guo [6].
For the pure compressible Euler equations, by contrast, shock formation is an intrinsic feature. As a hyperbolic system of conservation laws, the Euler system develops shocks even from smooth initial data. Thus the Boltzmann–Euler limit must ultimately be understood beyond the lifespan of classical Euler solutions, in regimes where the limiting fluid profile contains shock waves and contact discontinuities.
A complete kinetic theory of shock formation would have to connect the pre-shock smooth Euler-limit regime with the post-shock kinetic layer regime. Such a theory would require a simultaneous description of the emerging Euler discontinuity, the inner Boltzmann shock layer, and its dynamically selected location. For the fluid equations themselves, shock formation from smooth data has been studied in depth, from the classical one-dimensional theory to modern multidimensional works such as those of Christodoulou [7], Luk–Speck [8], and Buckmaster–Shkoller–Vicol [9], [10], among others. There has also been recent progress on the interaction between shock formation and small viscous regularization, for instance in the works of Chaturvedi–Graham [11] and Anderson–Chaturvedi–Graham [12]. At the kinetic level, however, a corresponding result that passes through the shock formation time and connects the smooth Euler limit to the emerging Boltzmann shock layer appears to remain largely open.
The limitation of smooth-limit theories is also consistent with a more critical viewpoint, advocated by Slemrod, according to which the Boltzmann-to-Euler passage beyond the smooth regime may face a genuine viscosity–capillarity obstruction [13]–[15].2 Building on the exact summation of the Chapman–Enskog expansion for Grad-type moment systems by Gorban–Karlin [16], Slemrod emphasized that the passage from the Boltzmann equation to the compressible Euler equations beyond the smooth regime is not a straightforward continuation of the pre-shock theory. In particular, once shocks or other nonsmooth structures are present, higher-gradient corrections cannot simply be regarded as negligible: the limiting process may retain a viscosity–capillarity mechanism of Korteweg type, and the capillarity contributions need not vanish in the sense of distributions.
This viewpoint should, in the authors’ view, be distinguished from a negative statement about kinetic-to-Euler limits themselves. In a different incompressible scaling, the previous work Bae-Kim [17] justifies the Boltzmann–Euler closure beyond the class of smooth classical Euler flows, without using either a Hilbert expansion or a Chapman–Enskog expansion. The argument relies instead on the exact macroscopic balance laws, together with quantitative estimates on the kinetic closure defects. These estimates show that the non-hydrodynamic moments vanish in the limit, and hence that the limiting dynamics is governed by the incompressible Euler equations even in rough solution classes. Thus, for the purposes of the present discussion, the obstruction emphasized by Slemrod should be interpreted chiefly as a limitation of formal expansion methods in nonsmooth regimes, rather than as a general obstruction to kinetic-to-Euler limits.
The present paper develops a related but distinct non-expansion mechanism for the compressible post-shock regime. We do not study the formation of shocks from smooth Euler flows. Rather, the limiting Euler profile is already a Riemann wave: a discontinuous composite pattern containing shocks and a contact discontinuity. The problem is therefore to justify the Boltzmann–Euler limit after the inviscid dynamics has entered the nonsmooth regime.
This is precisely the regime in which the formal smooth-limit theories cease to be adequate. The difficulty is not only to show that the kinetic closure defects vanish. Across each shock, the Boltzmann solution resolves the Euler jump through an \(O(\kappa)\)-scale kinetic layer. This inner layer carries a translation mode: shifting the shock profile costs essentially no leading-order energy. Consequently, even a small imbalance in the conserved quantities can produce a non-negligible displacement of the shock location. The shock position is therefore not a parameter that can be fixed in advance; it must be selected dynamically as part of the limiting process.
We consider the one-dimensional Boltzmann equation \[\label{eq:bee0} f_t+\xi_1 f_x = \frac{1}{\kappa}\mathcal{N}(f,f),\tag{1}\] where \(\xi=(\xi_1,\xi_2,\xi_3)\in\mathbb{R}^3\), \(x\in\mathbb{R}\), and \(\mathcal{N}\) denotes the hard-sphere collision operator. After transforming to Lagrangian mass coordinates, which we still denote by \(x\), one obtains \[\label{eq:bslk} f_t+\frac{\xi_1-u_1}{v}f_x = \frac{1}{\kappa}\mathcal{N}(f,f)\tag{2}\] where the specific volume \(v=\rho^{-1}\). As the Knudsen number \(\kappa\to0\), the above equation is expected to converge to the one-dimensional compressible Euler system in Lagrangian coordinates: \[\label{eq:cesL} \begin{align} & v_t-u_{1x}=0,\\ & u_{1t}+p_x=0,\\ & u_{it}=0,\qquad i=2,3,\\ & \left(\theta+\frac{|u|^2}{2}\right)_t+(pu_1)_x=0. \end{align}\tag{3}\] In this setting, the natural limiting objects are Riemann solutions to 3 . The analysis of already-formed shocks in kinetic equations rests first on the existence and structure theory of kinetic shock profiles. For the Boltzmann equation, Caflisch and Nicolaenko constructed small-amplitude shock profile solutions [18], writing the profile as a singular perturbative expansion in the shock strength whose leading terms agree with the corresponding Navier–Stokes shock profile. A fundamental issue in using such profiles as genuine distribution functions is their nonnegativity; this was addressed by Liu and Yu [19] through a macro–micro decomposition and energy method for Boltzmann shock layers.
The kinetic shock-profile theory was further developed through the invariant-manifold approach of Liu–Yu and Pogan–Zumbrun for steady Boltzmann flows [20], [21]. This viewpoint treats the steady Boltzmann equation as an infinite-dimensional dynamical system in the spatial variable and provides a structural framework for kinetic layers connecting Maxwellian end states. More recently, Albritton–Bedrossian–Novack constructed weak shock profiles for the Landau equation [22], extending the kinetic shock-profile theory beyond the hard-sphere and angular-cutoff Boltzmann setting to the plasma collision model. These works provide the kinetic shock layers that underlie hydrodynamic-limit results with already-formed shocks and also serve as the profile building blocks in the present paper.
Building on the kinetic shock-profile theory, Yu studied the zero-Knudsen-number limit toward piecewise smooth Euler flows containing shock waves [23]. The formulation there is made, for simplicity, in a periodic spatial setting and on a fixed finite time interval, with a finite number of isolated noninteracting shock curves. The proof is based on a highly delicate matched-asymptotic construction: a generalized Hilbert expansion is constructed away from the shock curves, exact Boltzmann shock profiles are inserted in the shock layers, and the resulting approximate solution is corrected through conservation-law constraints and a macro–micro stability analysis. This method requires successive matching and cancellation of the residual macroscopic fluxes generated by the shock-layer patching, together with a careful bookkeeping of outgoing diffusion waves and shock-location corrections.
The complexity of this strategy reflects the intrinsic difficulty of the compressible shock regime. As emphasized by Slemrod, the passage from Boltzmann to compressible Euler beyond the smooth regime is not a straightforward continuation of the pre-shock theory: in the presence of discontinuities, higher-gradient corrections, kinetic layers, and the selection of the shock location become part of the limiting process. Therefore a shock-layer-corrected Hilbert expansion must justify, at the same time, the outer Euler expansion, the inner Boltzmann shock layer, the matching between them, the residual conservation defects produced by the patching, and the stability of the final corrected approximation. This makes the approach powerful but necessarily rather elaborate.
Another result particularly close to the Riemann-problem setting of the present paper is due to Huang, Wang, Wang, and Yang [24], who justified the Boltzmann–Euler limit for Riemann solutions containing a generic superposition of shock waves, rarefaction waves, and a contact discontinuity. Their proof is based on a carefully corrected approximate-wave construction: auxiliary hyperbolic waves with different backgrounds are introduced to capture the extra masses generated by the hyperbolic approximation of rarefaction waves and the diffusion approximation of contact discontinuities. The perturbation is then controlled by an energy method around this corrected approximate Riemann pattern. A limitation of this approach, however, is that convergence is formulated only away from the shock and initial layers. More precisely, neighborhoods of the shock front and the initial time are removed from the convergence region, on top of that, the convergence depends on the size of the removed neighborhoods. This reflects the structure of the method and the topology for convergence. The corrected approximate-wave construction is designed to control the macroscopic defects of the Riemann solution on the Euler scale, while the shock layer itself lives on the kinetic scale \[\frac{x-\sigma t}{\kappa}.\] Inside this layer, derivatives of the shock profile are of size \(O(\kappa^{-1})\), and the leading difficulty is the translation mode of the kinetic shock. The anti-derivative method, without time modulation of the shock location, does not provide direct control of the superposition of the shock and rarefaction waves inside the shock and initial layers.
The present paper develops a different approach. We do not rely on a shock-layer-corrected Hilbert expansion around a prescribed discontinuous Euler flow, nor do we use the anti-derivative method. Instead, our argument is based on a kinetic adaptation of the \(a\)-contraction method for shocks, together with BV compactness of the shifts and control of the shock layers and approximate waves in the limit. The \(a\)-contraction method was first developed in [25], [26] for the stability of Riemann shocks, and extended to the stability of large perturbations of viscous shocks for viscous conservation laws as in [27]–[33]. As an extension of the method to the study on the time-asymptotic stability of small perturbations of Riemann solutions for the Navier-Stokes system, we refer to [34]–[37]. Recently, in [38], the method was used to study Boltzmann equation 2 for the long-time behavior towards the superposition composed of viscous shock, rarefaction and viscous contact. The key idea of the \(a\)-contraction method combines the relative entropy method with suitable weight and shift to quantify the orbital stability of shock waves. The weight encodes the jump strength and characteristic speed of a shock, and the shift is defined through a modulation equation (for control of the translation modes of shock) at the energy estimates.
On the other hand, the relative entropy method alone is sufficient to establish the stability of regular solutions other than shocks. The relative entropy method was first introduced by Dafermos [39] and DiPerna [40] to prove the stability of Lipschitz solutions to the hyperbolic conservation laws endowed with a convex entropy. It was also used for stochastic particle systems [41]–[43] and later adapted to the kinetic framework in [44], [45]. In the kinetic setting, this method is naturally compatible with Lions’ notion of dissipative solutions and is tailored to weak–strong stability. For other applications of the method to studies of asymptotic limits, we refer to [46]–[56].
In our setting, the \(a\)-contraction method is combined with the macro–micro structure of the Boltzmann equation. The Boltzmann shock profiles are retained as part of the target profile, but their locations are not fixed by an order-by-order correction of a matched asymptotic expansion. This is a key difference from the shock-layer construction of Yu, where the insertion of inner Boltzmann shock profiles into an outer Hilbert expansion creates residual macroscopic fluxes, and the shock locations must be corrected along the construction together with outgoing diffusion waves in order to restore the conservation constraints.
Here, by contrast, the shock locations are encoded by dynamically determined Shifts. The Shifts are selected through modulation equations to produce the coercive damping needed to control the translation modes of the shocks. Thus the shock shift in the present paper is not a bookkeeping correction in a formal expansion, but a coercive unknown of the stability estimate. The remaining kinetic errors are then controlled by the microscopic dissipation of the linearized Boltzmann operator.
Thus, our result should not be viewed as an implementation of the generalized Hilbert-expansion construction for another wave pattern, nor as an energy method based on anti-derivatives.
In this paper, we justify the hydrodynamic limit from 2 to 3 for generic Riemann solutions containing shocks, more precisely for composite waves consisting either of a \(1\)-shock, a \(2\)-contact discontinuity, and a \(3\)-shock, or of a \(1\)-rarefaction wave, a \(2\)-contact discontinuity, and a \(3\)-shock. Our result shows that, for suitably well-prepared initial data and sufficiently small wave strength, the corresponding Boltzmann solution exists globally and converges in \(L^2\), as \(\kappa\to0\), to the local Maxwellian associated with the Riemann solution. In the presence of shock components, the limiting profile must be tracked by suitable dynamical shifts, and the convergence is quantitative on every finite time interval.
Theorem 1 (Informal statements of Theorem 2 and Theorem 3). Consider a Riemann solution of the compressible Euler system 3 consisting of a \(1\)-shock, a \(2\)-contact discontinuity, and a \(3\)-shock, with sufficiently small total wave strength. Then, for suitably well-prepared initial data and sufficiently small Knudsen number \(\kappa>0\), the corresponding solution to the Boltzmann equation 2 exists globally and converges, as \(\kappa\to0\), to the local Maxwellian associated with the Riemann solution where the shock components are tracked by shifts \(X^0(t)\) as locally BV functions of time, more precisely, for any \(T>0\), \[\int_0^T \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|f^\kappa-M_{X^0}[v^E,u^E,\theta^E]\bigr|^2 \,d\xi\,dx\,dt \longrightarrow 0 \qquad\text{as }\kappa\to0,\] where \(M^{X^0}[v^E,u^E,\theta^E]\) denotes the Maxwellian associated with the Riemann solution containing shocks shifted by \(X^0\).
As a consequence, when the Riemann solution is a single shock, our general estimate yields a global quantitative estimate for the shock, not merely a local away-from-the-shock convergence theorem. The dependence on the distance to the location of modulated shock wave is explicit as \(y=\sigma \tau+X^\kappa(\tau)\), with an exponential tail at the kinetic scale \(\kappa\), as follows.
To formulate this consequence, let \(M^{E,\kappa}(\tau,y,\xi)\) be the Maxwellian associated with the Riemann shock whose location is modulated by the shift \(X^\kappa(\tau)\): \[M_{E,\kappa}(\tau,y,\xi) := \begin{cases} M_-(\xi), & y\le \sigma \tau+X^\kappa(\tau),\\[1mm] M_+(\xi), & y> \sigma \tau+X^\kappa(\tau). \end{cases}\]
Corollary 1 (Informal statement of Theorem 3). For a sufficiently small single shock and suitably well-prepared initial data, the corresponding Boltzmann solution converges to the Maxwellian associated with the Riemann shock, with the shock location modulated by a suitable time-dependent shift. More precisely, for every finite time interval \([0,T]\), \[\begin{align} \left\| f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \le C\,\kappa + C e^{-c|y-\sigma \tau-X^\kappa(\tau)|/\kappa}, \qquad (\tau,y)\in[0,T]\times\mathbb{R}. \end{align}\] In particular, the convergence is uniform on every region staying a fixed positive distance from the modulated shock wave.
We now describe the main difficulties and the main ideas of the proof. The first difficulty is the presence of shock waves in the limiting Euler profile. Across a shock, the limiting Maxwellian is discontinuous, and therefore the Boltzmann solution cannot converge uniformly through the shock layer. Moreover, the shock location is not fixed at the level of the kinetic perturbation. Even a small amount of mass, momentum, or energy imbalance can produce a displacement of the shock wave. For this reason the limiting profile must be modulated by time-dependent shifts.
We first normalize the Boltzmann equation with \(\kappa=1\) as in 9 . Since the Boltzmann equation contains microscopic degrees of freedom that are invisible at the Euler level, we use the macro–micro decomposition around the local Maxwellian to write \[f=M+G,\] and further decompose the microscopic part \(G\) relative to the shock profiles. Here, the fluid state associated to the Maxwellian \(M\) satisfies the Navier-Stokes-Fourier-type system 20 coupled with microscopic variables. The macro–micro decomposition is also used to write the Boltzmann shock \(F^{S_i}=M^{S_i}+ G^{S_i}\). The coercivity of the linearized collision operator supplies the basic microscopic dissipation, while the higher-order estimates close the terms involving derivatives of the microscopic component.
The key idea for controlling the macroscopic part of the perturbation is based on the a-contraction method. We consider a shock-adapted weight \(a(t,x)\) as in 39 and study the weighted relative entropy \[\int_{\mathbb{R}} a(t,x)\eta(U|\bar U)(t,x)\,dx,\] where \(\eta(U|\bar U)\) is the relative entropy between the fluid state \(U=(v,u,\theta)\) and the composite approximate wave \(\bar U=(\bar v,\bar u,\bar\theta)\) as in 58 . As in 60 , the evolution of the weighted relative entropy produces the modulation part \[\sum_{i\in\{1,3\}} \dot{X}_i(t)Y_i(t),\] the bad terms \(\mathcal{J}^{ {bad}}\), the good terms \(\mathcal{J}^{ {good}}\), and the kinetic part \(\mathcal{J}^{ {kinetic}}\). Based on the \(a\)-contraction method, the terms localized by derivatives of shock or weight in \(\mathcal{J}^{ {bad}}\) are controlled by the modulation part with suitable shift and the diffusion from \(\mathcal{J}^{ {good}}\). To control the contact discontinuity, we consider the associated viscous contact wave constructed in [57]. The contact component contributes Gaussian space-time weights of the form \[(1+t)^{-1} \exp\left(-\frac{c|x|^2}{1+t}\right),\] which cannot simply be absorbed by the shock dissipation. These terms are handled by a separate weighted estimate and by the decay properties of the viscous contact wave. On the other hand, the interaction of the waves is not easy to control, since the 1-shock and 3-shock are respectively shifted by different shifts. This requires that the locations of the two shocks are well-separated as in 46 . On top of that, based on this separation, we need to localize the diffusion term by the cutoff (as in 41 ), by which all the localized bad terms can be controlled by localized dissipation terms via the \(a\)-contraction method.
Since the fluid system 20 is coupled with the microscopic part, the above relative entropy estimates for the macroscopic variables should be coupled with microscopic energy-dissipation estimates for the kinetic remainder. Those
estimates will be performed under the a priori smallness assumption on the perturbation, as in Proposition 1. The a priori estimates provide stability of the viscous waves,
as in [38]. However, to get the desired singular limit, we need a careful layer analysis and BV compactness of shifts after scaling back to the \(\kappa\)-scaled equation 2 .
The proof is organized as follows. Section 2 states the main theorem and the well-preparedness assumptions. Section 3 collects the necessary preliminaries on the macro–micro decomposition, viscous contact waves, and Boltzmann shock profiles. Section 4
constructs the composite approximate wave and introduces the perturbation system, the dynamical shifts, and the main a priori proposition. Section 5 proves the main theorem assuming the a priori proposition, including the global continuation argument, the
rescaling to the original Knudsen number, and the convergence to the shifted Riemann solution. Section 6 establishes the low-order weighted relative-entropy estimates. Section 7 proves the higher-order macroscopic and microscopic estimates. Section 8
completes the proof of the main a priori proposition. Section 9 records the single-shock consequence and the rarefaction–contact–shock extension.
In this subsection, we describe the composite Euler waves that arise as the limiting profiles and the corresponding shifted local Maxwellians.
Fix a constant right end state \[U_+:=(v_+,u_{+},\theta_+)\in \mathbb{R}_+\times\mathbb{R}^3\times\mathbb{R}_+, \qquad u_+ := (u_{1+},0,0).\] For sufficiently small wave strength \(\delta>0\), let \[U^E=(v^E,u^E,\theta^E)(t,x)\] be a Riemann solution to the one-dimensional compressible Euler system 3 , connecting the left state \[U_-:=(v_-,u_{-},\theta_-), \qquad u_- := (u_{1-},0,0)\] to \(U_+\) through two intermediate states \(U_*\) and \(U^*\), with \[\delta:=|\theta_+-\theta_-|.\] We shall consider the following two wave patterns:
a superposition of a \(1\)-rarefaction wave, a \(2\)-contact discontinuity, and a \(3\)-shock wave;
a superposition of a \(1\)-shock wave, a \(2\)-contact discontinuity, and a \(3\)-shock wave.
We denote by \[U_{R_1}^E,\qquad U_C^E,\qquad U_{S_1}^E,\qquad U_{S_3}^E\] the corresponding elementary Euler wave patterns, whenever they are present. Thus, in case (a), \[U^E = U_{R_1}^E + U_C^E + U_{S_3}^E - U_* - U^*,\] whereas in case (b), \[U^E = U_{S_1}^E + U_C^E + U_{S_3}^E - U_* - U^*,\] where \[U_* = (v_*,u_*,\theta_*), \quad U^* = (v^*,u^*,\theta^*), \quad u_* = (u_{1*},0,0), \quad u^* = (u_1^*,0,0).\]
Let \(M[U]\) denote the local Maxwellian associated with the fluid state \(U=(v,u,\theta)\). In the presence of shock waves, the limiting profile is described up to suitable dynamical shifts along the shock components only. To denote a function \(f\) shifted by \(h\), we use the notation: \[f^{-h}(x)= f(x-h).\] So, for simplicity, we denote: for a shift function \(X_3=X_3(t)\), \[\label{eq:def-shifted-profile-rs} U^{X_3} := U_{R_1}^E + U_C^E + \bigl(U_{S_3}^E\bigr)^{-X_3} - U_* - U^*,\tag{4}\] and \[\label{eq:def-shifted-maxwellian-rs} M_{X_3}[U^E] := M[U^{X_3}],\tag{5}\] for the rarefaction–contact–shock case.
Similarly, for shift functions \(X_1=X_1(t)\), \(X_3=X_3(t)\) and \(X=(X_1,X_3)\), we denote \[\label{eq:def-shifted-profile-ss} U^{X} := \bigl(U_{S_1}^E\bigr)^{-X_1} + U_C^E + \bigl(U_{S_3}^E\bigr)^{-X_3} - U_* - U^*,\tag{6}\] and \[\label{eq:def-shifted-maxwellian-ss} M_{X}[U^E] := M[U^{X}],\tag{7}\] for the shock–contact–shock case.
In addition, let \(f^{S_3}\) denote the \(3\)-Boltzmann shock profile connecting the two Maxwellians \(M[U^*]\) and \(M[U_+]\). In the shock–contact–shock case, we also denote by \(f^{S_1}\) the \(1\)-Boltzmann shock profile connecting \(M[U_-]\) and \(M[U_*]\).
We next specify the class of admissible initial data for the Boltzmann equation 2 . Let \[U_0^E(x):=U^E(0,x)\] be the initial Riemann profile. We shall consider families of nonnegative smooth initial data \[\{f_0^\kappa\}_{\kappa>0}\] on \(\mathbb{R}_x\times\mathbb{R}_\xi^3\) such that for a sufficiently small constant \(\varepsilon_1>0\), \[\begin{align} & \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f^\kappa_0-M[U_0^E]|^2}{M_\#}\,d\xi\,dx + \kappa^2 \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f^\kappa_{0t}|^2+|f^\kappa_{0x}|^2}{M_\#}\,d\xi\,dx \notag\\ &\qquad + \kappa^4 \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f^\kappa_{0xx}|^2+|f^\kappa_{0tx}|^2}{M_\#}\,d\xi\,dx \le \kappa \varepsilon_1^2. \label{eq:initic2-main} \end{align}\tag{8}\] Here \(M_\#:=M[U_\#]\) is a fixed global Maxwellian. We refer to 8 as the well-preparedness condition. The appearance of the time derivatives \(f^\kappa_{0t}\) and \(f^\kappa_{0tx}\) reflects the higher-order compatibility built into the perturbative framework.
Remark 1. In Theorem 2, a upper bound of \(\varepsilon _1\) will be chosen to be small, which ensures the global existence of solution \(f^\kappa\) for each \(\kappa\). More precisely, after normalizing 8 , \(f_0(t,x,\xi):=f^\kappa_{0}(\kappa t, \kappa x, \xi)\) satisfies \[\begin{align} \label{eq:initda} \mathcal{E}_{\mathrm{ini}}^2 := & \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f_0-M[U_0^E]|^2}{M_\#}\,d\xi\,dx + \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f_{0t}|^2+|f_{0x}|^2}{M_\#}\,d\xi\,dx \nonumber\\ &\qquad + \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f_{0xx}|^2+|f_{0tx}|^2}{M_\#}\,d\xi\,dx \le \varepsilon_1^2. \end{align}\qquad{(1)}\] This small quantity (uniform-in-\(\kappa\)) related to \(f_0\) as the normalized initial datum of 9 , will control the initial quantity \(\mathcal{E}(0)\) appeared in the a priori estimates of Proposition 1 up to small constants as in 49 . Therefore, this small quantity is important to impose the smallness of \(\mathcal{E}(0)\) for the a priori estimates, by which the global existence of strong solutions to the Boltzmann equation 9 is guaranteed. This is why we impose the well-preparedness condition 8 as above.
We now state the precise form of the hydrodynamic limit theorem.
Theorem 2 (Hydrodynamic limit near a shock–contact–shock profile). Fix a constant end state \[U_+:=(v_+,u_{+},\theta_+)\in \mathbb{R}_+\times\mathbb{R}^3\times\mathbb{R}_+, \qquad u_+ := (u_{1+},0,0).\] Then there exist positive constants \(\varepsilon_0\), \(\delta_0\), and \(\kappa_0\), together with a global Maxwellian \(M_\#\), such that the following statement holds.
Let \(0<\delta\le \delta_0\), and let \[U^E=(v^E,u^E,\theta^E)(t,x)\] be a Riemann solution to the one-dimensional compressible Euler system 3 , connecting \[U_-:=(v_-,u_{-},\theta_-), \, \quad u_- :=(u_{1-},0,0) \quad \text{to} \quad U_+,\] through two intermediate states \(U_*\) and \(U^*\), with total wave strength \[\delta=\delta_1+\delta_C+\delta_3.\] where \(\delta_C\) the strength of the contact discontinuity, \(\delta_1:=|v_--v_*|\) the strength of the 1-shock wave and \(\delta_3:=|v^*-v_+|\) the strength of the 3-shock wave. Assume that \(U^E\) is a superposition of a \(1\)-shock wave, a \(2\)-contact discontinuity, and a \(3\)-shock wave. For each \(0<\varepsilon_1\le \varepsilon_0\) and \(0<\kappa\le \kappa_0\), let \(f_0^\kappa\) be a nonnegative smooth initial datum satisfying the well-preparedness condition 8 .
Then, there exists a unique solution \(f^\kappa\) to the Boltzmann equation 2 on a time interval \([0,T]\), where \(T>0\) is arbitrary. Moreover, there exist \[X_1^0,X_3^0\in BV([0,T])\] and families of shifts \(\{X_1^\kappa\}_{\kappa>0}\) and \(\{X_3^\kappa\}_{\kappa>0}\) such that, up to extraction of a subsequence, \[X_i^\kappa \to X_i^0 \qquad \text{in } L^1(0,T), \qquad i=1,3,\] and \[\begin{align} \label{eq:hlmt1-main} &\int_0^T \iint_{\mathbb{R}\times\mathbb{R}^3} \left|f^\kappa-M_{X^0}[U^E]\right|^2 \,d\xi\,dx\,dt\nonumber\\ &\qquad\le C\kappa\bigl((\varepsilon_1+\delta_0)^2+\delta_0^{1/2}\bigr)T + C\delta_C\,\kappa^{1/2}T^{3/2} + C\delta_0^2\sum_{i=1,3}\|X_i^\kappa-X_i^0\|_{L^1(0,T)}. \end{align}\qquad{(2)}\] Here, the positive constant \(C\) is independent of \(\kappa\) and \(T\).
We now turn to the normalized problem obtained by scaling out the Knudsen number. More precisely, although the original Boltzmann equation was introduced in 1 and 2 with Knudsen number \(\kappa\), throughout the a priori analysis we work with the rescaled equation in which \(\kappa=1\). The dependence on the original Knudsen number will be recovered at the end of the proof by a scaling argument.
Thus, in this section we consider the one-dimensional Boltzmann equation in Eulerian coordinates \[\label{eq:bee} f_t+\xi_1 f_x = \mathcal{N}(f,f),\tag{9}\] where \(\xi=(\xi_1,\xi_2,\xi_3)\in\mathbb{R}^3\), \(x\in\mathbb{R}\), and \(\mathcal{N}\) is the hard-sphere collision operator: \[\label{eq:Qdef} \mathcal{N}(g,h)(\xi) = \iint_{\mathbb{R}^3\times \mathbb{S}_+^2} |(\xi-\xi_*)\cdot \Omega| \Bigl(g(\xi')h(\xi_*')-g(\xi)h(\xi_*)\Bigr) \,d\Omega\,d\xi_*,\tag{10}\] where \[\label{eq:postcoll} \xi'+\xi_*'=\xi+\xi_*, \qquad |\xi'|^2+|\xi_*'|^2=|\xi|^2+|\xi_*|^2,\tag{11}\] and \[\mathbb{S}_+^2 := \left\{ \Omega\in\mathbb{S}^2:(\xi-\xi_*)\cdot\Omega\ge0 \right\}.\]
Passing from Eulerian to Lagrangian coordinates, the coordinate is still denote by \(x\), 9 becomes \[\label{eq:bel} f_t+\frac{\xi_1-u_1}{v}f_x = \mathcal{N}(f,f),\tag{12}\] where \(u_1\) is the first component of the fluid velocity and \(v=\rho^{-1}\) is the specific volume.
For a solution \(f(t,x,\xi)\) of 12 , we employ the macro–micro decomposition relative to the local Maxwellian; see [58]. The macroscopic part corresponds to the fluid variables, namely the density \(\rho\), the momentum \(\rho u\), and the total energy \(\rho\bigl(e+\frac{|u|^2}{2}\bigr)\), where \(u=(u_1,u_2,u_3)\) denotes the fluid velocity and \(e\) the internal energy.
More precisely, let \(M\) be the normalized local Maxwellian, and define \[\label{eq:mami} P_0^{[M]} g := \sum_{i=0}^4 \langle g,\chi^{[M]}_i\rangle \chi^{[M]}_i, \qquad P_1^{[M]} g := g-P_0^{[M]} g,\tag{13}\] where \[\label{eq:chi} \chi_0=\frac{M}{\sqrt{\rho}}, \qquad \chi_i=\frac{\xi_i-u_i}{\sqrt{R\theta\,\rho}}M \quad (i=1,2,3), \qquad \chi_4= \frac{1}{\sqrt{6\rho}} \left( \frac{|\xi-u|^2}{R\theta}-3 \right)M,\tag{14}\] and \[\label{eq:inner} \langle g,h\rangle_{M} := \int_{\mathbb{R}^3}\frac{g(\xi)h(\xi)}{M(\xi)}\,d\xi.\tag{15}\]
Here, \(P_0^{[M]}\) and \(P_1^{[M]}\) denote the macroscopic and microscopic projections, respectively. We write \[f=M+G, \qquad M:=P_0^{[M]}f, \qquad G:=P_1^{[M]}f.\]
In addition, we also define useful norms by
\[\begin{align} \bigl\lVert g\bigr\rVert_{M_\#}^2 := \int_{\mathbb{R}^3} \frac{|g|^2}{M_\#} d\xi, \qquad \bigl\lVert g\bigr\rVert_{\nu,M_\#}^2 := \int_{\mathbb{R}^3} \frac{(1+|\xi|)|g|^2}{M_\#} d\xi \end{align}\]
where \(M_\#\) is a given global Maxwellian. We sometimes set \(\bigl\lVert\cdot\bigr\rVert_{L^2_{\xi}(M_\#)}:=\bigl\lVert\cdot\bigr\rVert_{M_\#}\) to emphasize the function-space norm.
Integrating 12 against the collisional invariants \[1,\quad \xi_1,\quad \xi_2,\quad \xi_3,\quad \frac{|\xi|^2}{2},\] we obtain the macroscopic fluid-type system \[\label{eq:NSl} \begin{align} & v_t-u_{1x}=0,\\ & u_{1t}+p_x=-\int \xi_1^2 G_x\,d\xi,\\ & u_{it}=-\int \xi_1\xi_i G_x\,d\xi,\qquad i=2,3,\\ & \left(\theta+\frac{|u|^2}{2}\right)_t+(pu_1)_x = -\int \frac{1}{2}\xi_1|\xi|^2 G_x\,d\xi. \end{align}\tag{16}\]
On the other hand, substituting \(f=M+G\) into 12 and applying the microscopic projection, we obtain \[\label{eq:mile} \begin{align} G_t -\frac{u_1}{v}G_x +\frac{1}{v}P_1^{[M]}(\xi_1 M_x) +\frac{1}{v}P_1^{[M]}(\xi_1 G_x) = L_MG+\mathcal{N}(G,G), \end{align}\tag{17}\] where \[L_MG:=\mathcal{N}(M,G)+\mathcal{N}(G,M)\] is the linearized collision operator around \(M\).
Applying \(L_M^{-1}\) to 17 , we decompose the microscopic part into a diffusion term and a remainder term: \[\label{eq:G} G = \frac{1}{v}L_M^{-1}\Bigl(P_1^{[M]}(\xi_1M_x)\Bigr) +\Pi_1,\tag{18}\] with \[\label{eq:Ger} \Pi_1 := L_M^{-1} \left( G_t -\frac{u_1}{v}G_x +\frac{1}{v}P_1^{[M]}(\xi_1G_x) -\mathcal{N}(G,G) \right).\tag{19}\]
Substituting 18 into 16 , we arrive at the fluid-type system \[\label{eq:NSF1} \begin{align} & v_t-u_{1x}=0,\\ & u_{1t}+p_x = \frac{4}{3}\left(\frac{\mu(\theta)u_{1x}}{v}\right)_x -\int \xi_1^2 \Pi_{1x}\,d\xi,\\ & u_{it} = \left(\frac{\mu(\theta)u_{ix}}{v}\right)_x -\int \xi_1\xi_i \Pi_{1x}\,d\xi, \qquad i=2,3,\\ & \left(\theta+\frac{|u|^2}{2}\right)_t+(pu_1)_x = \left(\frac{\alpha_{\rm{th}}(\theta)\theta_x}{v}\right)_x +\frac{4}{3}\left(\frac{\mu(\theta)u_1u_{1x}}{v}\right)_x \\ &\qquad \qquad \qquad \qquad \qquad +\sum_{i=2}^3 \left(\frac{\mu(\theta)u_i u_{ix}}{v}\right)_x -\int \frac{1}{2}\xi_1|\xi|^2 \Pi_{1x}\,d\xi. \end{align}\tag{20}\] Here \(\mu(\theta)\) and \(\alpha_{\rm{th}}(\theta)\) denote the viscosity and heat conductivity, respectively. We define \(\gamma:=\frac{\alpha_{\rm{th}}(\theta)}{\mu(\theta)}\). For the hard sphere, \(\frac{\alpha_{\rm{th}}(\theta)}{\mu(\theta)}\) is constant([59]), so we will use the following notation:
For the viscous contact wave, following [60] and [57], we consider the self-similar solution \(\Theta^{\mathrm{sim}}\) to the nonlinear diffusion equation \[\begin{align} \begin{aligned} & \Theta_t^{\mathrm{sim}} = \frac{9p_*}{10} \left( \frac{\alpha_{\rm{th}}(\Theta^{\mathrm{sim}})\Theta_x^{\mathrm{sim}}}{\Theta^{\mathrm{sim}}} \right)_x,\\ & \Theta^{\mathrm{sim}}(t,-\infty)=\theta_*, \qquad \Theta^{\mathrm{sim}}(t,\infty)=\theta^* \end{aligned} \end{align}\] where \(U_*=(v_*,u_*,\theta_*)\) is the left state and \(U^*=(v^*,u^*,\theta^*)\) is the right state. Using this self-similar profile, we define the viscous contact wave \((v^C,u^C,\theta^C)(t,x)\) by \[\begin{align} \begin{aligned}\label{eq:ctident0} & v^C(t,x):=\frac{2\Theta^{\mathrm{sim}}(t,x)}{3p_*},\\ & u_1^C(t,x):=u_{1*}+\frac{3\alpha_{\rm{th}}(\Theta^{\mathrm{sim}})\Theta_x^{\mathrm{sim}}}{5\Theta^{\mathrm{sim}}},\\ & u_i^C(t,x)\equiv 0,\qquad i=2,3,\\ & \theta^C(t,x):=\Theta^{\mathrm{sim}}(t,x). \end{aligned} \end{align}\tag{21}\] Then \((v^C,u^C,\theta^C)\) satisfies \[\begin{align} \begin{aligned}\label{eq:ctident} & v_t^C-u_{1x}^C=0,\\ & u_{1t}^C+p_x^C=\frac{4}{3}\left(\frac{\mu(\theta^C)u_{1x}^C}{v^C}\right)_x+Q_1^C,\\ & u_i^C=0,\qquad i=2,3,\\ & \theta_t^C+p^C u_{1x}^C = \left(\frac{\alpha_{\rm{th}}(\theta^C)\theta_x^C}{v^C}\right)_x +\frac{4}{3}\mu(\theta^C)\frac{(u_{1x}^C)^2}{v^C} +Q_2^C, \end{aligned} \end{align}\tag{22}\] where \[\begin{align} \begin{aligned} Q_1^C := u_{1t}^C-\frac{4}{3}\left(\frac{\mu(\theta^C)u_{1x}^C}{v^C}\right)_x,\;\;\; Q_2^C := -\frac{4}{3}\mu(\theta^C)\frac{(u_{1x}^C)^2}{v^C}. \end{aligned} \end{align}\] Morevoer, \[\begin{align} \label{eq:contact-Q-bounds} Q_1^C=O(1)\delta_C(1+t)^{-3/2}e^{-c_0x^2/(1+t)}, \qquad Q_2^C=O(1)\delta_C(1+t)^{-2}e^{-2c_0x^2/(1+t)}. \end{align}\tag{23}\]
The construction above is standard; see [57]. For the convenience of the reader, we record the Gaussian bounds needed below.
Lemma 1. Let \[\delta_C:=|\theta^*-\theta_*|.\] Then there exists a positive constant \(c_0>0\) such that \[\begin{align} \label{eq:Theta-sim-x} |\Theta_x^{\mathrm{sim}}(t,x)| \le C\delta_C(1+t)^{-1/2}e^{-c_0x^2/(1+t)}, \end{align}\qquad{(3)}\] and consequently we have 23 : \[\begin{align} \notag Q_1^C=O(1)\delta_C(1+t)^{-3/2}e^{-c_0x^2/(1+t)}, \qquad Q_2^C=O(1)\delta_C(1+t)^{-2}e^{-2c_0x^2/(1+t)}. \end{align}\]
Lemma 2 ([60]). Let \(\delta_C\) denote the stregnth of the contact discontinuity as \[\delta_C := |v^*-v_*|\] The viscous contact discontinuity \((v^C,u_1^C,\theta^C)(t,x)\) defined in 21 satisfies \[\begin{align} \label{eq:ctident1} (v^C-v_*,u_1^C - u_{1*}, \theta^C -\theta_*) & = O(1) \delta_C e^{-\frac{c_0x^2}{1+t}}, && \forall x<0, \notag\\ (v^C-v^*,u_1^C - u_1^*, \theta^C - \theta^*) & = O(1) \delta_C e^{-\frac{c_0x^2}{1+t}}, && \forall x>0, \notag\\ (\partial_x^n v^C, \partial_x^n \theta^C)(t,x) &= O(1)\delta_C (1+t)^{\frac{n}{2}}e^{-\frac{c_0x^2}{1+t}}, && \forall x\in \mathbb{R}, \quad n=1,2,\ldots, \notag\\ \partial_x^n u_1^C(t,x) &= O(1) \delta_C(1+t)^{-\frac{1+n}{2}}e^{-\frac{c_0x^2}{1+t}}, && \forall x\in \mathbb{R}, \quad n=1,2, \ldots, \end{align}\qquad{(4)}\] where \(c_0>0\) is a constant.
It follows in particular from Lemma 2 that \[(v^C,u_1^C,\theta^C)(t,x) \to (v_*,u_{1*},\theta_*) \quad \text{as }x\to -\infty,\]
and \[(v^C,u_1^C,\theta^C)(t,x) \to (v^*,u_1^*,\theta^*) \quad \text{as }x\to +\infty.\] Furthermore, restoring the dependence on the heat-conductivity coefficient in terms of the Knudsen number \(\kappa\), the viscous contact wave satisfies, for any \(1\le p<\infty\), \[\label{eq:contma} \Bigl\| (v^C,u_1^C,\theta^C)(t,\cdot)-(v^c,u_1^c,\theta^c)(t,\cdot) \Bigr\|_{L^p(\mathbb{R})}\le C\delta_C\kappa^{\frac{1}{2p}}(1+t)^{\frac{1}{2p}}.\tag{24}\] Consequently, for each fixed \(T>0\), \[\begin{align} \label{eq:hydrolimit-contact} (v^C,u_1^C,\theta^C)\longrightarrow (v^c,u_1^c,\theta^c)\quad \text{in }L^\infty(0,T;L^p(\mathbb{R})) \quad \text{as }\kappa \to 0. \end{align}\tag{25}\] Here \((v^c,u_1^c,\theta^c)\) is the inviscid contact discontinuity. This convergence should be understood on finite time intervals. Over large time scales the diffusive spreading of the viscous contact discontinuity may become non-negligible.
We briefly recall the mechanism behind these standard results. The steady Boltzmann profile equation may be viewed as an infinite-dimensional dynamical system near an end Maxwellian. For small-amplitude shocks, one constructs a local invariant/center manifold around equilibrium and reduces the profile equation to a finite-dimensional slow dynamics whose leading part is the corresponding compressible Navier–Stokes shock ODE. The Boltzmann shock profile is then obtained as a heteroclinic orbit on this reduced manifold connecting the two end states. In this framework, the exponential decay, monotonicity, and higher-derivative bounds for the macroscopic profile follow from the reduced shock dynamics, while the bounds for the microscopic component \(G^{S_i}\) and the remainder \(\Pi_1^{S_i}\) are recovered through the macro–micro decomposition and the coercive invertibility of the linearized collision operator on the microscopic subspace; see [20], [61].
For \(i=1,3\), set \[z_i:=x-\sigma_i t,\] where \(\sigma_i\) is the \(i\)-th shock speed. We denote by \[F^{S_i}(t,x,\xi):=F^{S_i}(z_i,\xi) = F^{S_i}(x-\sigma_i t,\xi)\] the traveling profile of the steady \(i\)-th Boltzmann shock profile in Lagrangian coordinates. Hence, when acting on \(F^{S_i}\), we have \[\partial_t=-\sigma_i\partial_{z_i}, \qquad \partial_x=\partial_{z_i}.\] Then \(F^{S_i}\) satisfies \[\label{drtbmvki} -\sigma_i (F^{S_i})_{z_i} -\frac{u_1^{S_i}-\xi_1}{v^{S_i}}(F^{S_i})_{z_i} = \mathcal{N}(F^{S_i},F^{S_i}).\tag{26}\] Here, the end states are \[\begin{align} & F^{S_1}(-\infty,\xi)=M[U_-], \qquad F^{S_1}(+\infty,\xi)=M[U_*], \qquad u_*=(u_{1*},0,0),\\ & F^{S_3}(-\infty,\xi)=M[U^*], \qquad F^{S_3}(+\infty,\xi)=M[U_+], \qquad u^*=(u^{1*},0,0). \end{align}\]
As in 13 , we decompose the shock profile into its macroscopic and microscopic parts: \[\begin{align} & M^{S_i}(z,\xi):=M_{[v^{S_i},u^{S_i},\theta^{S_i}]}(z,\xi),\\ & F^{S_i}=M^{S_i}+G^{S_i}, \qquad M^{S_i}=P_0^{[M^{S_i}]}F^{S_i}, \qquad G^{S_i}:=P_1^{[M^{S_i}]}F^{S_i}, \end{align}\] where \[\begin{align} & P_0^{[M^{S_i}]}g:=\sum_{k=0}^4\langle g,\chi_k^{S_i^0}\rangle_{M^{S_i}}\chi_k^{S_i^0}, \qquad P_1^{[M^{S_i}]}g:=g-P_0^{[M^{S_i}]}g, \\ & \chi_0^{S_i^0}=\frac{M^{S_i}}{\sqrt{\rho^{S_i}}}, \qquad \chi_j^{S_i^0}=\frac{\xi_j-u_j^{S_i}}{\sqrt{R\theta^{S_i}\rho^{S_i}}}M^{S_i}, \quad j=1,2,3,\\ & \chi_4^{S_i^0} = \frac{1}{\sqrt{6\rho^{S_i}}} \left( \frac{|\xi-u^{S_i}|^2}{R\theta^{S_i}}-3 \right)M^{S_i}. \end{align}\]
Set \(P_j:=P_j^{[M]},\,P_j^{S_i^0}:=P_j^{[M^{S_i}]}\) for \(j=0,1\). By the macro–micro decomposition, the macroscopic part satisfies the fluid-type system \[\label{eq:NSls} \begin{align} & -\sigma_i (v^{S_i})_{z_i}-(u_1^{S_i})_{z_i}=0,\\ & -\sigma_i (u_1^{S_i})_{z_i}+(p^{S_i})_{z_i} = \frac{4}{3}\left(\frac{\mu(\theta^{S_i})u_{1z_i}^{S_i}}{v^{S_i}}\right)_{z_i} -\int \xi_1^2(\Pi_1^{S_i})_{z_i}\,d\xi,\\ & u_j^{S_i}\equiv0,\qquad j=2,3,\\ & -\sigma_i (\theta^{S_i})_{z_i}+p^{S_i}(u_1^{S_i})_{z_i} = \left(\frac{\alpha_{\rm{th}}(\theta^{S_i})\theta_{z_i}^{S_i}}{v^{S_i}}\right)_{z_i} +\frac{4}{3}\mu(\theta^{S_i})\frac{(u_{1z_i}^{S_i})^2}{v^{S_i}} \\ &\qquad \qquad \qquad \qquad \qquad \qquad \qquad -\int \xi_1\left(\frac{|\xi|^2}{2}-u_1^{S_i}\xi_1\right)(\Pi_1^{S_i})_{z_i}\,d\xi, \end{align}\tag{27}\] while the microscopic part satisfies \[\label{eq:Gers} \begin{align} & -\sigma_i G_{z_i}^{S_i} -\frac{u_1^{S_i}}{v^{S_i}}G_{z_i}^{S_i} +\frac{1}{v^{S_i}}P_1^{S_i^0}(\xi_1 G_{z_i}^{S_i}) +\frac{1}{v^{S_i}}P_1^{S_i^0}(\xi_1 M_{z_i}^{S_i}) = L_{M^{S_i}}G^{S_i}+\mathcal{N}(G^{S_i},G^{S_i}),\\ & G^{S_i} = \frac{1}{v^{S_i}}(L_{M^{S_i}})^{-1}\!\Bigl(P_1^{S_i^0}(\xi_1M_{z_i}^{S_i})\Bigr) +\Pi_1^{S_i},\\ & \Pi_1^{S_i} := (L_{M^{S_i}})^{-1} \left( -\sigma_i G_{z_i}^{S_i} -\frac{u_1^{S_i}}{v^{S_i}}G_{z_i}^{S_i} +\frac{1}{v^{S_i}}P_1^{S_i^0}(\xi_1G_{z_i}^{S_i}) -\mathcal{N}(G^{S_i},G^{S_i}) \right). \end{align}\tag{28}\]
The following properties of the shock profile will be used later.
Lemma 3 ([24],[20]). For a given right end state \((v_R,u_{1R},0,0,\theta_R)\), there exists a constant \(C>0\) such that the following holds. For any left end state \((v_L,u_{1L},0,0,\theta_L)\) sufficiently close to \((v_R,u_{1R},0,0,\theta_R)\) and connected to it by an \(i\)-shock curve, \(i=1,3\), with shock strength \[\delta_i:=|v_R-v_L| \sim |u_{1R}-u_{1L}| \sim |\theta_R-\theta_L|,\] there exists a unique shock profile \[(v^{S_i}(z),u^{S_i}(z),\theta^{S_i}(z))\] associated with [eq:bse]. Moreover, \[\begin{align} & (v^{S_1})'(z)<0,\qquad (u_1^{S_1})'(z)<0,\qquad (\theta^{S_1})'(z)>0,\\ & (v^{S_3})'(z)>0,\qquad (u_1^{S_3})'(z)<0,\qquad (\theta^{S_3})'(z)<0, \qquad \forall z\in\mathbb{R},\\ & |(v^{S_i}(z)-v_L,\;u_1^{S_i}(z)-u_{1L},\;\theta^{S_i}(z)-\theta_L)| \le C\delta_i e^{-C\delta_i|z|}, \qquad z<0,\\ & |(v^{S_i}(z)-v_R,\;u_1^{S_i}(z)-u_{1R},\;\theta^{S_i}(z)-\theta_R)| \le C\delta_i e^{-C\delta_i|z|}, \qquad z>0,\\ & |((v^{S_i})'(z),(u_1^{S_i})'(z),(\theta^{S_i})'(z))| \le C\delta_i^2 e^{-C\delta_i|z|}, \qquad \forall z\in\mathbb{R},\\ & |\partial_z^k ((v^{S_i})(z),(u_1^{S_i})(z),(\theta^{S_i})(z))| \le C\delta_i^{k-1}|((v^{S_i})'(z),(u_1^{S_i})'(z),(\theta^{S_i})'(z))|. \end{align}\]
Lemma 4 ([24],[20]). Under the assumptions of Lemma 3, there exists a unique Boltzmann shock profile \(F^{S_i}(z,\xi)\) solving [eq:bse]. Moreover, \[\begin{align} & \left(\int \frac{(1+|\xi|)|G^{S_i}|^2}{M_\#}\,d\xi\right)^{1/2} \le C\delta_i^2 e^{-C\delta_i|z|},\\ & \left(\int \frac{(1+|\xi|)|\partial_z^k G^{S_i}|^2}{M_\#}\,d\xi\right)^{1/2} \le C\delta_i^k \left(\int \frac{(1+|\xi|)|G^{S_i}|^2}{M_\#}\,d\xi\right)^{1/2},\\ & \left|\int \xi_1\varphi_\ell(\xi)\Pi_1^{S_i}\,d\xi\right| \le C\delta_i \left(\int \frac{(1+|\xi|)|G^{S_i}|^2}{M_\#}\,d\xi\right)^{1/2}, \qquad \ell=1,4,\\ & \left|\int \xi_1\varphi_\ell(\xi)(\Pi_1^{S_i})_x\,d\xi\right| \le C\delta_i^2 \left(\int \frac{(1+|\xi|)|G^{S_i}|^2}{M_\#}\,d\xi\right)^{1/2}, \qquad \ell=1,4,\\ & \int \xi_1\varphi_\ell(\xi)\Pi_1^{S_i}\,d\xi=0, \qquad \ell=2,3, \end{align}\] where \(M_\#\) is a fixed global Maxwellian close to the shock profile, and \[\varphi_\ell(\xi)=\xi_\ell,\quad \ell=1,2,3, \qquad \varphi_4(\xi)=\frac{|\xi|^2}{2}.\]
Lemma 5 ([38]). Under the assumptions of Lemmas 3 and 4, the following hold: \[\begin{align} & |(u_1^{S_1})'-\sigma_*(v^{S_1})'| \le C\delta_1 |(v^{S_1})'|, \qquad |(u_1^{S_3})'+\sigma^*(v^{S_3})'| \le C\delta_3 |(v^{S_3})'|,\\ & |(\theta^{S_1})'+p_*(v^{S_1})'| \le C\delta_1 |(v^{S_1})'|, \qquad |(\theta^{S_3})'+p^*(v^{S_3})'| \le C\delta_3 |(v^{S_3})'|, \end{align}\] and \[\begin{align} & \left| \frac{p^{S_1}-p_-}{v^{S_1}-v_-} - \frac{p^{S_1}-p_*}{v^{S_1}-v_*} - \frac{5p_*}{9v_*^2} \left( \frac{10\mu(\theta_*)-9\alpha_{\rm{th}}(\theta_*)}{10\mu(\theta_*)+3\alpha_{\rm{th}}(\theta_*)}+3 \right) \right| \le C\delta_1^2,\\ & \left| \frac{p^{S_3}-p_+}{v^{S_3}-v_+} - \frac{p^{S_3}-p^*}{v^{S_3}-v^*} - \frac{5p^*}{9(v^*)^2} \left( \frac{10\mu(\theta^*)-9\alpha_{\rm{th}}(\theta^*)}{10\mu(\theta^*)+3\alpha_{\rm{th}}(\theta^*)}+3 \right) \right| \le C\delta_3^2 \end{align}\] where \(p_*=\frac{2\theta_*}{3v_*}\), \(p^*=\frac{2\theta^*}{3v^*}\), \(\sigma_*=\sqrt{\frac{5p_*}{3v_*}}\), and \(\sigma^*=\sqrt{\frac{5p^*}{3v^*}}\).
We now introduce the composite approximate wave, consisting of the viscous contact wave and the two viscous shock waves shifted by the dynamical shifts \(X_i(t)\), \(i=1,3\), to be determined later. For convenience, for any macroscopic profile \(h^{S_i}\) we write \[\bigl(h^{S_i}\bigr)^{-X_i}(t,x) := h^{S_i}(x-\sigma_i t-X_i(t)), \qquad i=1,3\] and the microscopic profile \(g^{S_i}\) we write \[\bigl(g^{S_i}\bigr)^{-X_i}(t,x,\xi) := g^{S_i}(x-\sigma_i t-X_i(t),\xi), \qquad i=1,3\] We define \[\label{eq:unvar} \begin{align} \bar v(t,x) &:= \bigl(v^{S_1}\bigr)^{-X_1}(t,x) + v^C(t,x) + \bigl(v^{S_3}\bigr)^{-X_3}(t,x) -v_*-v^*,\\ \bar u(t,x) &:= (\bar u_1, 0, 0)(t,x), \\ \bar u_1(t,x) &:= \bigl(u_1^{S_1}\bigr)^{-X_1}(t,x) + u_1^C(t,x) + \bigl(u_1^{S_3}\bigr)^{-X_3}(t,x) -u_{1*}-u_1^*,\\ \bar\theta(t,x) &:= \bigl(\theta^{S_1}\bigr)^{-X_1}(t,x) + \theta^C(t,x) + \bigl(\theta^{S_3}\bigr)^{-X_3}(t,x) -\theta_*-\theta^*,\\ \bar U &:= \bigl(\bar v, \bar u_1,0,0,\bar \theta \bigr),\\ \bar p (t,x)&:= p(\bar v(t,x), \bar \theta(t,x)),\\ p^{S_{i},-X_{i}} (t,x)&:=\bigl(p^{S_{i}}\bigr)^{-X_{i}}(t,x),\qquad i=1,3,\\ \bar M(t,x,\xi) &:=M[\bar U](\xi),\\ \bar f(t,x,\xi) &:= \bar M(t,x,\xi) + \bigl(G^{S_1}\bigr)^{-X_1}(t,x,\xi) + \bigl(G^{S_3}\bigr)^{-X_3}(t,x,\xi). \end{align}\tag{29}\]
We record the elementary identity \[\label{eq:rbsws} \begin{align} \partial_t\left( \bigl(v^{S_i}\bigr)^{-X_i}\right) &= -(\sigma_i+\dot{X}_i(t))\,\partial_x \left( \bigl(v^{S_i}\bigr)^{-X_i} \right)\\ &= -\dot{X}_i(t)\,\partial_x \left(\bigl(v^{S_i}\bigr)^{-X_i}\right) +\partial_x \left(\bigl(u_1^{S_i}\bigr)^{-X_i}\right), \qquad i=1,3, \end{align}\tag{30}\] where in the second equality we used the profile equation \[-\sigma_i (v^{S_i})'-(u_1^{S_i})'=0.\] By combining the equations for the viscous contact wave and the two shifted shock profiles(See 27 , 22 ), we obtain that the composite ansatz \((\bar v,\bar u,\bar\theta)\) satisfies
\[\begin{align} \label{eq:ansasy} &\bar v_t +\dot{X}_1(t)\partial_x \bigl(v^{S_{1}}\bigr)^{-X_{1}} +\dot{X}_3(t)\partial_x \bigl(v^{S_{3}}\bigr)^{-X_{3}} -\bar u_{1x} =0,\nonumber\\ &\bar u_{1t} +\dot{X}_1(t)\partial_x \bigl(u_1^{S_{1}}\bigr)^{-X_{1}} +\dot{X}_3(t)\partial_x \bigl(u_1^{S_{3}}\bigr)^{-X_{3}} +\bar p_x\nonumber\\ &\qquad \qquad = \frac{4}{3}\left(\frac{\mu(\bar\theta)\bar u_{1x}}{\bar v}\right)_x +Q_1 -\sum_{i\in\{1,3\}}\int \xi_1^2\partial_x\bigl(\Pi_1^{S_{i}}\bigr)^{-X_{i}}\,d\xi,\nonumber\\ &\bar u_i=0,\qquad i=2,3,\nonumber\\ &\bar\theta_t +\dot{X}_1(t)\partial_x \bigl(\theta^{S_{1}}\bigr)^{-X_{1}} +\dot{X}_3(t)\partial_x \bigl(\theta^{S_{3}}\bigr)^{-X_{3}} +\bar p\,\bar u_{1x}\nonumber\\ &\,= \left(\frac{\alpha_{\rm{th}}(\bar\theta)\bar\theta_x}{\bar v}\right)_x +\frac{4}{3}\mu(\bar\theta)\frac{\bar u_{1x}^2}{\bar v} +Q_2 -\sum_{i\in\{1,3\}}\int \xi_1\left(\frac{|\xi|^2}{2}-\bigl(u_1^{S_i}\bigr)^{-X_i}\xi_1\right)\partial_x \bigl(\Pi_1^{S_{i}}\bigr)^{-X_{i}}\,d\xi, \end{align}\tag{31}\] where \[\label{eq:Q1Q2} \begin{align} Q_1 &:= Q_1^C +\Bigl( \bar p -p^{S_{1},-X_{1}} -p^{S_{3},-X_{3}} -p^C \Bigr)_x\\ &\qquad +\frac{4}{3}\left( \frac{\mu\bigl(\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\bigr)\bigl(\partial_x\bigl(u_{1}^{S_{1}}\bigr)^{-X_{1}}\bigr)}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}} + \frac{\mu\bigl(\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}\bigr)\bigl(\partial_x\bigl(u_1^{S_{3}}\bigr)^{-X_{3}}\bigr)}{\bigl(v^{S_{3}}\bigr)^{-X_{3}}} + \frac{\mu(\theta^C)u_{1x}^C}{v^C} - \frac{\mu(\bar\theta)\bar u_{1x}}{\bar v} \right)_x\\ &=: Q_1^C + Q_1^I, \end{align}\tag{32}\] and \[\label{eq:Q2Q2} \begin{align} Q_2 &:= Q_2^C + \Bigl( \bar p\,\bar u_{1x} -p^{S_{1},-X_{1}}\bigl(\partial_x\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}\bigr) -p^{S_{3},-X_{3}}\bigl(\partial_x\bigl(u_1^{S_{3}}\bigr)^{-X_{3}}\bigr) -p^Cu_{1x}^C \Bigr)\\ &\quad +\left( \frac{\alpha_{\rm{th}}\bigl(\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\bigr)\bigl(\partial_x\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\bigr)}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}} + \frac{\alpha_{\rm{th}}\bigl(\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}\bigr)\bigl(\partial_x\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}\bigr)}{\bigl(v^{S_{3}}\bigr)^{-X_{3}}} + \frac{\alpha_{\rm{th}}(\theta^C)\theta_x^C}{v^C} - \frac{\alpha_{\rm{th}}(\bar\theta)\bar\theta_x}{\bar v} \right)_x\\ &\quad +\frac{4}{3}\mu(\theta^C)\frac{(u_{1x}^C)^2}{v^C} +\frac{4}{3}\mu\bigl(\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\bigr)\frac{\bigl(\partial_x\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}\bigr)^2}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}} +\frac{4}{3}\mu\bigl(\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}\bigr)\frac{\bigl(\partial_x\bigl(u_1^{S_{3}}\bigr)^{-X_{3}}\bigr)^2}{\bigl(v^{S_{3}}\bigr)^{-X_{3}}} \\ &\quad -\frac{4}{3}\mu(\bar\theta)\frac{\bar u_{1x}^2}{\bar v}\\ &=: Q_2^C + Q_2^I \end{align}\tag{33}\]
To implement the relative entropy method, we introduce the perturbation variables around the composite approximate wave 29 . Define \[\label{eq:pevar} \begin{align} \phi(t,x) &:=v(t,x)-\bar v(t,x),\\ \psi (t,x) &= (\psi_1,\psi_2,\psi_3)(t,x):=u(t,x)-\bar u(t,x),\\ \zeta (t,x) &:= \theta(t,x)-\bar \theta(t,x), \\ \widetilde{f}(t,x,\xi) &:=f(t,x,\xi) - \bigl(F^{S_1}\bigr)^{-X_1}(t,x,\xi) - \bigl(F^{S_3}\bigr)^{-X_3}(t,x,\xi),\\ \widetilde{G}(t,x,\xi) &:= G(t,x,\xi) - \bigl(G^{S_1}\bigr)^{-X_1}(t,x,\xi) - \bigl(G^{S_3}\bigr)^{-X_3}(t,x,\xi). \end{align}\tag{34}\] We summarize the notation used in the perturbation formulation. The function \(f\) denotes the dynamic solution to the Boltzmann equation, whereas \(\bar f\) denotes the composite approximate distribution. We denote by \(\bar M\) the local Maxwellian associated with the composite macroscopic profile. After subtracting the shock contributions, we write \(\widetilde{f}\) for the shock-subtracted distribution and \(\widetilde{G}\) for the corresponding shock-subtracted microscopic perturbation.
Subtracting the composite ansatz system 31 from the full system, we obtain \[\label{eq:pesy1} \begin{align} & \phi_t -\dot{X}_1(t)\left(\bigl(v^{S_1}\bigr)^{-X_1}\right)_x -\dot{X}_3(t)\left(\bigl(v^{S_3}\bigr)^{-X_3}\right)_x -\psi_{1x}=0,\\ & \psi_{1t} -\dot{X}_1(t)\left(\bigl(u_1^{S_1}\bigr)^{-X_1}\right)_x -\dot{X}_3(t)\left(\bigl(u_1^{S_3}\bigr)^{-X_3}\right)_x +(p-\bar p)_x\\ & \qquad= \frac{4}{3}\left( \frac{\mu(\theta)u_{1x}}{v} - \frac{\mu(\bar\theta)\bar u_{1x}}{\bar v} \right)_x -Q_1 -\int \xi_1^2\Bigl(\Pi_1-\bigl(\Pi_1^{S_1}\bigr)^{-X_1}-\bigl(\Pi_1^{S_3}\bigr)^{-X_3}\Bigr)_x\,d\xi, \end{align}\tag{35}\] \[\label{eq:pesy2} \begin{align} & \psi_{it} = \left(\frac{\mu(\theta)\psi_{ix}}{v}\right)_x -\int \xi_1\xi_i \Pi_{1x}\,d\xi, \qquad i=2,3,\\ & \zeta_t -\dot{X}_1(t)\left(\bigl(\theta^{S_1}\bigr)^{-X_1}\right)_x -\dot{X}_3(t)\left(\bigl(\theta^{S_3}\bigr)^{-X_3}\right)_x +\bigl(pu_{1x}-\bar p\,\bar u_{1x}\bigr)\\ & \qquad= \left( \frac{\alpha_{\rm{th}}(\theta)\theta_x}{v} - \frac{\alpha_{\rm{th}}(\bar\theta)\bar\theta_x}{\bar v} \right)_x +\frac{4}{3}\left( \frac{\mu(\theta)u_{1x}^2}{v} - \frac{\mu(\bar\theta)\bar u_{1x}^2}{\bar v} \right) +\frac{\mu(\theta)(\psi_{2x}^2+\psi_{3x}^2)}{v} -Q_2\\ & \qquad\quad -\int \xi_1\frac{|\xi|^2}{2}\Bigl(\Pi_1-\bigl(\Pi_1^{S_1}\bigr)^{-X_1}-\bigl(\Pi_1^{S_3}\bigr)^{-X_3}\Bigr)_x\,d\xi +\sum_{j=2}^3 \psi_j\int \xi_1\xi_j\Pi_{1x}\,d\xi\\ & \qquad\quad +\left( u_1\int \xi_1^2\Pi_{1x}\,d\xi -\sum_{i\in\{1,3\}}\bigl(u_1^{S_i}\bigr)^{-X_i}\int \xi_1^2\left(\bigl(\Pi_1^{S_i}\bigr)^{-X_i}\right)_x\,d\xi \right), \end{align}\tag{36}\] and \[\label{eq:pesy3} \begin{align} \widetilde{G}_t-L_M\widetilde{G} &= \dot{X}_1(t)\left(\bigl(G^{S_1}\bigr)^{-X_1}\right)_x +\dot{X}_3(t)\left(\bigl(G^{S_3}\bigr)^{-X_3}\right)_x +\frac{u_1}{v}\widetilde{G}_x -\frac{1}{v}P_1(\xi_1\widetilde{G}_x)\\ &\quad +\sum_{i\in\{1,3\}}\left(\frac{u_1}{v}-\frac{(u_1^{S_i})^{-X_i}}{(v^{S_i})^{-X_i}}\right)\left(\bigl(G^{S_i}\bigr)^{-X_i}\right)_x\\ &\quad -\sum_{i\in\{1,3\}}\left( \frac{1}{v}P_1\bigl(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) -\frac{1}{(v^{S_i})^{-X_i}}P_1^{S_i}\bigl(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) \right)\\ &\quad -\frac{1}{v}P_1(\xi_1 M_x) +\sum_{i\in\{1,3\}}\frac{1}{(v^{S_i})^{-X_i}}P_1^{S_i}\bigl(\xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}\bigr) \\ &\quad +\mathcal{N}(\widetilde{G},\widetilde{G}) +\mathcal{N}\bigl((G^{S_1})^{-X_1},\widetilde{G}\bigr) +\mathcal{N}\bigl(\widetilde{G},(G^{S_1})^{-X_1}\bigr) \\ &\quad +\mathcal{N}\bigl((G^{S_3})^{-X_3},\widetilde{G}\bigr) +\mathcal{N}\bigl(\widetilde{G},(G^{S_3})^{-X_3}\bigr)\\ &\quad +\mathcal{N}\bigl((G^{S_1})^{-X_1},(G^{S_3})^{-X_3}\bigr) +\mathcal{N}\bigl((G^{S_3})^{-X_3},(G^{S_1})^{-X_1}\bigr) \\ &\quad +\sum_{i=1,3}\bigl(L_M-L_i^S\bigr)\bigl(G^{S_i}\bigr)^{-X_i} \end{align}\tag{37}\]
where
\[\begin{align} L_i^{S_i}:=L_{\left(M^{S_i}\right)^{-X_i}},\quad i=1,3, \quad P_j^{S_i} := P_j^{[\bigl(M^{S_{i}}\bigr)^{-X_{i}}]}, \quad i=1,3,\,j=0,1. \end{align}\]
To handle the two shock waves, we introduce weight functions associated with the \(1\)-shock and the \(3\)-shock; see [34], [62]. Define \[\label{eq:aweight} \begin{align} a_1(z)&:=1+\frac{1}{\sqrt{\delta_1}}\bigl(v^{S_1}(z)-v_-\bigr),\\ a_3(z)&:=1+\frac{1}{\sqrt{\delta_3}}\bigl(v^{S_3}(z)-v^*\bigr), \end{align}\tag{38}\] where \[\delta_1:=|v_--v_*|, \qquad \delta_3:=|v_+-v^*|\] denote the strengths of the \(1\)-shock and the \(3\)-shock, respectively.
For the shifted shock profiles, we set \[\label{eq:wefun} a(t,x) := a_1(x-\sigma_1 t-X_1(t)) + a_3(x-\sigma_3 t-X_3(t)) -1.\tag{39}\] Before defining the shift coefficients, we recall the constants \(p_*, p^*, \sigma_*,\sigma^*\), which are fixed throughout the argument. \[\begin{align} p_* = \frac{2\theta_*}{3v_*},\quad p^*=\frac{2\theta^*}{3v^*},\quad \sigma_* = \sqrt{\frac{5p_*}{3v_*}},\quad \sigma^*=\sqrt{\frac{5p^*}{3v^*}}. \end{align}\] These constants are chosen according to the admissible range of the shock strengths and the associated shock speeds, and they will be used in the definition of the coefficients \(\mathfrak m_1\) and \(\mathfrak m_3\) below. We now define the dynamical shifts \((X_1,X_3)\) by the system of ordinary differential equations \[\label{eq:shift} \begin{align} \dot{X}_1(t) &= -\frac{\mathfrak m_1}{\delta_1} \int_{\mathbb{R}} a \left( \left((u_1^{S_1})^{-X_1}\right)_x\psi_1 + \frac{\left((v^{S_1})^{-X_1}\right)_x\,\overline{p}}{\overline{v}}\phi + \frac{\left((\theta^{S_1})^{-X_1}\right)_x}{\overline{\theta}}\zeta \right)\,dx,\\ \dot{X}_3(t) &= -\frac{\mathfrak m_3}{\delta_3} \int_{\mathbb{R}} a \left( \left((u_1^{S_3})^{-X_3}\right)_x\psi_1 + \frac{\left((v^{S_3})^{-X_3}\right)_x\,\overline{p}}{\overline{v}}\phi + \frac{\left((\theta^{S_3})^{-X_3}\right)_x}{\overline{\theta}}\zeta \right)\,dx,\\ X_1(0)&=X_3(0)=0, \end{align}\tag{40}\] where the constants \(\mathfrak m_i\), \(i=1,3\) are defined as below.
\[\begin{align} \mathfrak m_1 := \frac{20}{3}\frac{p_*}{\sigma_*^3v_*^2}\frac{5+3\gamma}{10+3\gamma}, \qquad \mathfrak m_3:=\frac{20}{3}\frac{p^*}{(\sigma^*)^3(v^*)^2}\frac{5+3\gamma}{10+3\gamma}. \end{align}\]
To separate the two shock regions, we introduce the cutoff functions \(\varphi_1\) and \(\varphi_3\) by \[\label{eq:intske} \varphi_1(t,x) := \begin{cases} 1, & x\le \dfrac{X_1(t)+\sigma_1 t}{2},\\[2mm] 0, & x\ge \dfrac{X_3(t)+\sigma_3 t}{2},\\[2mm] \text{linearly decreasing from 1 to 0}, & \dfrac{X_1(t)+\sigma_1 t}{2}<x<\dfrac{X_3(t)+\sigma_3 t}{2}, \end{cases}\tag{41}\]
and
\[\label{eq:intske1} \varphi_3(t,x):=1-\varphi_1(t,x).\tag{42}\]
To prove the global existence on the time interval \([0,T]\), we shall close the following a priori estimate. Define
\[\label{eq:mic2} \begin{align} & \widetilde{G}_{\text{rem}} := \widetilde{G}-\widetilde{G}_C, \qquad \widetilde{G}_C := \frac{3}{2v\theta} L_M^{-1}P_1 \left[ \xi_1M \left( \xi_1u_{1x}^C+\frac{|\xi-u|^2}{2\theta}\theta_x^C \right) \right]. \end{align}\tag{43}\] and \[\label{eq:priass} \begin{align} \mathcal{E}(T)^2 := \sup_{t\in[0,T]} \Biggl\{ &\|(\phi,\psi,\zeta)(t)\|_{H^1_x}^2 +\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{M_\#}^2\,+\bigl\lVert\widetilde{G}_x\bigr\rVert_{M_\#}^2\,dx\\ &\qquad+\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_t\bigr\rVert_{M_\#}^2\,+\bigl\lVert\widetilde{f}_{xx}\bigr\rVert_{M_\#}^2\,+\bigl\lVert\widetilde{f}_{tx}\bigr\rVert_{M_\#}^2\,dx\Biggr\}. \end{align}\tag{44}\]
The main a priori estimate is stated as follows.
Proposition 1. Let \(U_+:=(v_+,u_{1+},0,0,\theta_+)\in\mathbb{R}_+\times\mathbb{R}^3\times\mathbb{R}_+\). Then there exist positive constants \(\delta_0\), \(\varepsilon\), and \(C\), together with a global Maxwellian \(M_\#:=M[U_\#]\), independent of \(T\), such that the following holds.
Suppose that \((U,f)=(v,u,\theta,f)\) solves 20 and 12 on \([0,T]\) for some \(T>0\). Set \(\delta:=\delta_1+\delta_C+\delta_3\). For any \(0<\delta<\delta_0\), let \((\bar v,\bar u,\bar\theta)\) be the composite wave defined in 29 , where the dynamical shifts \(X_1\) and \(X_3\) are the absolutely continuous solutions to 40 associated with the weight function 39 . Assume that \[\begin{align} \label{eq:prioriass} \mathcal{E}(T)^2\le \varepsilon^2. \end{align}\qquad{(5)}\] Then \[\label{eq:pries} \begin{align} \mathcal{E}(T)^2 &+\sum_{i=1,3}\int_0^T \delta_i |\dot{X}_i(t)|^2\,dt +\sum_{i=1,3}\int_0^T \mathcal{G}_i^S(t)\,dt\\ &+\sum_{|\beta|=1}\int_0^T \|\partial^\beta(\phi,\psi,\zeta)(t)\|_{L^2_x}^2\,dt+\int_0^T \|(\phi_{xx},\psi_{xx},\zeta_{xx},\phi_{xt},\psi_{xt},\zeta_{xt})(t)\|_{L^2_x}^2\,dt\\ &+\int_0^T\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \,dx\,dt\\ &\le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr), \end{align}\qquad{(6)}\] where \[\label{eq:skGt} \mathcal{G}_i^S(t) := \int_{\mathbb{R}} \bigl|\partial_x(v^{S_i})^{-X_i}(t,x)\bigr| \,|\varphi_i(t,x)|^2 \,|(\phi,\psi,\zeta)(t,x)|^2\,dx, \qquad i=1,3,\qquad{(7)}\] and \(\varphi_i\) is defined in 41 .
The remainder of the paper is devoted to the proof of Proposition 1. The global existence argument is then completed by combining Proposition 1 with the local-in-time existence result proved in Appendix.
First, by the a priori assumption ?? together with the Sobolev embedding, we have \[\bigl\|(\phi,\psi,\zeta)\bigr\|_{L^\infty((0,T)\times \mathbb{R})} \le C\varepsilon\] In particular, \(v,u,\theta \in L^\infty((0,T)\times\mathbb{R})\).
Next, using the ODE 40 and Lemma 3, we obtain \[\begin{align} |\dot{X}_1(t)|+|\dot{X}_3(t)| &\le \sum_{i\in\{1,3\}} \frac{C}{\delta_i} \bigl\|(\phi,\psi,\zeta)\bigr\|_{L^\infty(\mathbb{R})}\int_\mathbb{R}|\partial_x (\bigl(v^{S_{i}}\bigr)^{-X_{i}})|\,dx \notag\\ &\le C\bigl\|(\phi,\psi,\zeta)\bigr\|_{L^\infty(\mathbb{R})} \le C \varepsilon . \label{eq:shift-speed-bound} \end{align}\tag{45}\]
Hence, by taking \(\varepsilon>0\) sufficiently small, we may assume that \[|\dot{X}_1(t)|+|\dot{X}_3(t)| \le \varepsilon\] with \(\varepsilon\) small compared to the shock speeds. Since \(X_1(0)=X_3(0)=0\), it follows from 45 that \[X_1(t)\le -\frac{\sigma_1}{2}t, \qquad X_3(t)\ge -\frac{\sigma_3}{2}t, \qquad t>0.\] Equivalently, \[\begin{align} \label{eq:shiftsp1} X_1(t)+\sigma_1 t \le \frac{\sigma_1}{2} t,\qquad X_3(t)+\sigma_3 t \ge \frac{\sigma_3}{2} t, \qquad t>0. \end{align}\tag{46}\] This proves that the shifts are well-separated.
The following lemma quantifies the weak interaction between the two separated shock waves.
Lemma 6 ([62]). Assume \(X_1(t)\leq -\frac{\sigma_1}{2}t\) and \(X_3(t)\geq-\frac{\sigma_3}{2}t\). There exist positive constants \(\delta_0\) and \(C\) such that if \[\delta_1,\delta_C,\delta_3\in(0,\delta_0),\] then for all \(t>0\) and \(x\in\mathbb{R}\), \[\label{eq:intsk1} \begin{align} &\varphi_3(t,x)\,\bigl|\partial_x(v^{S_1})^{-X_1}(t,x)\bigr| \le C\delta_1^2 e^{-C\delta_1 t}, \quad \varphi_1(t,x)\,\bigl|\partial_x(v^{S_3})^{-X_3}(t,x)\bigr| \le C\delta_3^2 e^{-C\delta_3 t},\\ &\int_{\mathbb{R}}\varphi_3(t,x)\,\bigl|\partial_x(v^{S_1})^{-X_1}(t,x)\bigr|\,dx \le C\delta_1 e^{-C\delta_1 t}, \quad \int_{\mathbb{R}}\varphi_1(t,x)\,\bigl|\partial_x(v^{S_3})^{-X_3}(t,x)\bigr|\,dx \le C\delta_3 e^{-C\delta_3 t}. \end{align}\qquad{(8)}\]
Lemma 7 ([62]). Assume \(X_1(t)\leq -\frac{\sigma_1}{2}t\) and \(X_3(t)\geq-\frac{\sigma_3}{2}t\). There exists a positive constant \(C\), independent of \(T\), \(\delta_1\), \(\delta_3\), and \(\delta_C\), such that for all \(t\in[0,T]\), \[\begin{align} \label{eq:wave-interaction-L2} \left\| |\partial_x(v^{S_1})^{-X_1}| \,|(v^C-v_*,\theta^C-\theta_*)| \right\|_{L^2_x} &\le C\delta_1^{3/2}\delta_C e^{-C \delta_1 t}, \\ \label{eq:wave-interaction-L2b} \left\| |\partial_x(v^{S_1})^{-X_1}| \,|(v^{S_3}-v^*,\theta^{S_3}-\theta^*)^{-X_3}| \right\|_{L^2_x} &\le C\delta_1^{3/2}\delta_3 \bigl(e^{-C\delta_1 t}+e^{-C\delta_3 t}\bigr). \end{align}\] {#eq: sublabel=eq:eq:wave-interaction-L2,eq:eq:wave-interaction-L2b} Similarly, \[\begin{align} \label{eq:wave-interaction-L2-3} \left\| |\partial_x(v^{S_3})^{-X_3}| \,|(v^C-v^*,\theta^C-\theta^*)| \right\|_{L^2_x} &\le C\delta_3^{3/2}\delta_C e^{-C\delta_3 t}, \\ \label{eq:wave-interaction-L2-3b} \left\| |\partial_x(v^{S_3})^{-X_3}| \,|(v^{S_1}-v_*,\theta^{S_1}-\theta_*)^{-X_1}| \right\|_{L^2_x} &\le C\delta_3^{3/2}\delta_1 \bigl(e^{-C\delta_1 t}+e^{-C\delta_3 t}\bigr). \end{align}\] {#eq: sublabel=eq:eq:wave-interaction-L2-3,eq:eq:wave-interaction-L2-3b}
Lemma 8 (Derivative wave-interaction estimate). For \(|\alpha|=1,2\), there exists a positive constant \(C\), independent of \(T\), \(\delta_1\), \(\delta_3\), and \(\delta_C\), such that for all \(t\in[0,T]\), \[\begin{align} \label{eq:wave-interaction-derivative-1} &\int_{\mathbb{R}} \bigl|\partial_x^\alpha(v^C-v_*)\bigr|^2 \bigl|(v^{S_1})_x^{-X_1}\bigr|^2\,dx + \int_{\mathbb{R}} \bigl|\partial_x^\alpha\bigl((v^{S_3}-v^*)^{-X_3}\bigr)\bigr|^2 \bigl|(v^{S_1})_x^{-X_1}\bigr|^2\,dx \nonumber\\ &\qquad\le C\delta_1^{3} \delta_C^2 e^{-C\delta_1 t} + C\delta_1^3\delta_3^{2(|\alpha|+1)}\bigl(e^{-C\delta_3 t}+e^{-C\delta_1 t}\bigr). \end{align}\qquad{(9)}\] Similarly, \[\begin{align} \label{eq:wave-interaction-derivative-3} &\int_{\mathbb{R}} \bigl|\partial_x^\alpha(v^C-v^*)\bigr|^2 \bigl|(v^{S_3})_x^{-X_3}\bigr|^2\,dx + \int_{\mathbb{R}} \bigl|\partial_x^\alpha\bigl((v^{S_1}-v_*)^{-X_1}\bigr)\bigr|^2 \bigl|(v^{S_3})_x^{-X_3}\bigr|^2\,dx \nonumber\\ &\qquad\le C\delta_3^{3} \delta_C^2 e^{-C\delta_3 t} + C\delta_3^3\delta_1^{2(|\alpha|+1)}\bigl(e^{-C\delta_3 t}+e^{-C\delta_1 t}\bigr). \end{align}\qquad{(10)}\]
Proof. As in Lemma [lem:wave-interaction-L2], we split the real line and compute the wave interaction. Using Lemma [lem:bs] and ?? , we can obtain ?? and ?? . ◻
Lemma 9 (Wave-interaction estimate, [37]). Let \(X_i\) (\(i=1,\,3\)) be the shift defined by 40 and \(Q_i^I\)(\(i=1,\,2\)) be defined in 32 and 33 . There exists a positive constant \(C\), independent of \(T\), \(\delta_1\), \(\delta_3\), and \(\delta_C\), such that for all \(t\in[0,T]\), \[\label{eq:intskfull} \bigl\lVert Q_i^I\bigr\rVert_{L^2} \leq C\delta_1^{\frac{3}{2}}(\delta_3+\delta_C)e^{-C\delta_1t}+C\delta_3^{\frac{3}{2}}(\delta_1+\delta_C)e^{-C\delta_3t}\qquad{(11)}\]
We here complete the proof of Theorem 2 by combining the a priori estimates with the local existence. The proof of Proposition 1 will be handled in the subsequent sections.
To complete the continuation argument, we establish a local-in-time existence result around the unshifted composite approximate wave. Define \[\label{eq:lceans} \begin{bmatrix} \hat{v}\\ \hat{u}_1\\ \hat{u}_2\\ \hat{u}_3\\ \hat{\theta} \end{bmatrix}(t,x) := \begin{bmatrix} v^{S_1}(x-\sigma_1 t)+v^C(t,x)+v^{S_3}(x-\sigma_3 t)-v_*-v^*\\ u_1^{S_1}(x-\sigma_1 t)+u_1^C(t,x)+u_1^{S_3}(x-\sigma_3 t)-u_{1*}-u_1^*\\ 0\\ 0\\ \theta^{S_1}(x-\sigma_1 t)+\theta^C(t,x)+\theta^{S_3}(x-\sigma_3 t)-\theta_*-\theta^* \end{bmatrix},\tag{47}\] where two intermediate states \[U_* = (v_*,u_*,\theta_*), \quad U^* = (v^*,u^*,\theta^*), \quad u_*=(u_{1*},0,0), \quad u^*=(u^*_1,0,0)\] and let \[\label{eq:hatM} \hat{M}:=M[\hat{U}],\qquad \hat{U} :=(\hat{v},\hat{u},\hat{\theta}).\tag{48}\]
We shall use the following local existence result.
Proposition 2. For any sufficiently small constant \(R>0\), there exists a positive time \(T_{\mathrm{loc}}=T_{\mathrm{loc}}(R)\) such that the following holds. Define \(h:= f-\hat{M}\). Assume that \[\label{eq:lcext-ass} \sum_{|\alpha|+|\beta|\le2,\;|\beta|\le1} \Bigl\|\bigl\lVert\partial_x^\alpha\partial_t^\beta(f_0-\hat{M})\bigr\rVert_{M_\#} \Bigr\|_{L^2_x} \le \frac{R}{2}\qquad{(12)}\] for some global Maxwellian \(M_\#\). Then the Cauchy problem for the normalized Lagrangian Boltzmann equation 12 admits a unique nonnegative solution \(f\) on \([0,T_*]\) such that \[\label{eq:lcext-conc} \sup_{t\in[0,T_{\mathrm{loc}}]} \sum_{|\alpha|+|\beta|\le2,\;|\beta|\le1} \Bigl\|\bigl\lVert\partial_x^\alpha\partial_t^\beta \,h\bigr\rVert_{M_\#} \Bigr\|_{L^2_x} \le R.\qquad{(13)}\] Here, the time derivatives of \(f_0\) are understood through the Boltzmann equation evaluated at \(t=0\).
By the shift estimate 45 , \[\begin{align} \bigl\lVert v^{S_i}-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\bigr\rVert_{H^1}^2 \le& C \delta_i + \int_{-|X_i|}^0 (v^{S_i}-v_R)^2 dx + \int_0^{|X_i|}(v^{S_i}-v_L)^2 dx \\ \le& C\delta_i(1+t) \end{align}\] where \(v_R\) is the right state of \(i\)-shock and \(v_L\) is the left state of \(i\)-shock for \(i=1,3\). Therefore, in the continuation argument, all perturbation norms are understood with respect to the shifted composite profile \(\bar{U}\), not the unshifted profile \(\hat{U}\). This is legitimate because the local well-posedness and coercivity estimates are invariant under spatial translations of the shock profiles.
We now verify the smallness of the initial energy. Applying ?? at \(t=0\), gives \[\begin{align} \label{eq:pxt} \begin{aligned} \mathcal{E}(0)^2 &\le C\mathcal{E}_{\mathrm{ini}}^2 + C(\delta_1+\delta_C+\delta_3)^2 . \end{aligned} \end{align}\tag{49}\]
We first justify that the microscopic part can be controlled by \(f-\hat{M}\). Set \(U=(v,u,\theta)\), \(\hat{U}=(\hat{v},\hat{u}, \hat{\theta})\), and \(h= f-\hat{M}\). Since \(G=f-M[U]\) is microscopic part, \[\begin{align} \int_{\mathbb{R}^3} G\psi(\xi)\,d\xi =0,\qquad \psi=(1,\xi,|\xi|^2). \end{align}\] Hence \[\begin{align} \mathcal{A}(U) -\mathcal{A}(\hat{U}) = \int_{\mathbb{R}^3} h\,\psi(\xi)\,d\xi \qquad \mathcal{A}(U):=\int_{\mathbb{R}^3}M[U]\psi(\xi)\,d\xi . \end{align}\] The moment map \(\mathcal{A}\) is uniformly non-degenerate on the compact set under consideration; indeed, writing \(\rho=1/v\), \[\begin{align} |U-\hat{U}| \le C\Bigl|\int_{\mathbb{R}^3} h\, \psi(\xi)\, d\xi \Bigr| \le C \bigl\|h\bigr\|_{M_\#}. \end{align}\] Consequently, \[\begin{align} \bigl\lVert U-\hat{U}\bigr\rVert_{L_x^2}^2 \le C \bigl\lVert f-\hat{M}\bigr\rVert_{L^2_x(L_\xi^2(M_\#))}^2. \end{align}\] Moreover, since \[\begin{align} G = (f-\hat{M}) - (M[U]-\hat{M}), \end{align}\] the smooth dependence of the Maxwellian on \(U\) gives \[\begin{align} \int \bigl\lVert G\bigr\rVert_{M_\#}^2 dx \le C \bigl\lVert f-\hat{M}\bigr\rVert_{L_x^2(L_\xi(M_\#))}^2 \qquad (\text{by }\eqref{eq:Maxwellian-Lipschitz-single}) \end{align}\]
Note that \[\begin{align} \left\|f-\hat{M}\right\|_{L_x^2(L_\xi^2(M_\#))}^2 &\le \left\|f-M[U^E]+M[U^E]-\hat{M}\right\|_{L_x^2(L_\xi^2(M_\#))}^2\\ &\le \left\|f-M[U^E]\right\|_{L_x^2(L_\xi^2(M_\#))}^2 +\left\|M[U^E]-\hat{M}\right\|_{L_x^2(L_\xi^2(M_\#))}^2 \\ &\le \mathcal{E}_{\mathrm{ini}}^2 + C(\delta_1+\delta_C+\delta_3)^2 \end{align}\] at time \(t=0\). Similarly, we can apply for \(\partial^{\alpha}(U-\hat{U})\) where \(\partial^\alpha = \partial^{\alpha_0}_t\partial^{\alpha_1}_x\) and \(|\alpha|=|\alpha_0|+|\alpha_1|\le 2,\, |\alpha_0|\le 1\).
When \(|\alpha|=1\),
\[\begin{align} \Bigl|\int_{\mathbb{\mathbb{R}}^3} \partial^\alpha h \psi(\xi) d\xi \Bigr|&=\Bigl| D\mathcal{A}(U)\partial^\alpha U - D\mathcal{A}(\hat{U}) \partial^\alpha \hat{U} \Bigr| \\ &= \Bigl|D \mathcal{A}(U) \partial^\alpha(U-\hat{U}) + \bigl(D\mathcal{A}(U)-D\mathcal{A}(\hat{U})\bigr)\partial^\alpha \hat{U}\Bigr| \end{align}\] Since \(D\mathcal{A}\) is invertible, \[\begin{align} |\partial^\alpha(U-\hat{U})| &\le C\Bigl|\int_{\mathbb{\mathbb{R}}^3} \partial^\alpha h \psi(\xi) d\xi \Bigr| + |\partial^\alpha \hat{U}||D\mathcal{A}(U)-D\mathcal{A}(\hat{U})| \\ &\le C\Bigl|\int_{\mathbb{\mathbb{R}}^3} \partial^\alpha h \psi(\xi) d\xi \Bigr| + C(\delta_1+\delta_C+\delta_3)|U-\hat{U}|. \end{align}\] Therefore, \(|\alpha|=1\), \[\begin{align} \|\partial^\alpha(U-\hat{U})\|_{L_x^2}^2 \le C\left\|\partial^\alpha(f-\hat{M})\right\|_{L_x^2(L_\xi^2(M_\#))}^2 + C(\delta_1+\delta_C+\delta_3)^2 \left\|(f-\hat{M})\right\|_{L_x^2(L_\xi^2(M_\#))}^2 \end{align}\]
\[\begin{align} \left\|\partial^\alpha(f-\hat{M})\right\|_{L_x^2(L_\xi^2(M_\#))}^2 &\le \left\|\partial^\alpha f\right\|_{L_x^2(L_\xi^2(M_\#))}^2 +\left\|\partial^\alpha \hat{M}\right\|_{L_x^2(L_\xi^2(M_\#))}^2 \\ &\le \mathcal{E}_{\mathrm{ini}}^2 + C(\delta_1+\delta_C+\delta_3)^2 \end{align}\] at time \(t=0\). When \(|\alpha|=2\) and \(|\alpha_0|\le1\), these are controlled by \(f\) itself from the definition of \(\mathcal{E}(t)\), 44 . Combining the above estimates with the initial data ?? yields \[\begin{align} \label{eq:priass-2} \mathcal{E}(0)^2 \le C\varepsilon_1^2 + C(\delta_1+\delta_C+\delta_3)^2 . \end{align}\tag{50}\]
Now, we prove the global existence of the normalized solution. By the local-in-time existence result, Proposition 2, there exists a unique nonnegative solution on a short time interval. On the other hand, Proposition 1 yields an a priori estimate which improves the a priori bound in ?? , provided that the initial perturbation and the wave strengths are sufficiently small. Therefore, a standard continuity argument implies that the normalized solution can be continued globally in time on any interval \([0,T]\), and the estimate ?? holds uniformly on \([0,T]\).
In particular, the shifts \(X_1\) and \(X_3\) are absolutely continuous and satisfying 46 on every finite interval, and all estimates in Proposition 1 are available for arbitrary \(T>0\).
Let \(f\) denote the global normalized solution furnished by the global continuation argument above. For \(0<\kappa\le \kappa_0\), define the rescaled solution by \[\begin{align} f^\kappa(\tau,y,\xi):= f\!\left(\frac{\tau}{\kappa},\frac{y}{\kappa},\xi\right), \qquad \bar f^{\,\kappa}(\tau,y,\xi):= \bar f\!\left(\frac{\tau}{\kappa},\frac{y}{\kappa},\xi\right). \label{eq:rescaled-solution} \end{align}\tag{51}\] Then \(f^\kappa\) solves the Boltzmann equation 2 with Knudsen number \(\kappa\), and \(\bar f^{\,\kappa}\) is the corresponding rescaled composite approximate wave.
For the shifts, define \[\begin{align} X_i^\kappa(\tau):= \kappa X_i\!\left(\frac{\tau}{\kappa}\right), \qquad i=1,3. \label{eq:rescaled-shifts} \end{align}\tag{52}\]
Lemma 10. For every \(T>0\), \[\begin{align} \int_0^T\iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f^\kappa-\bar f^{\,\kappa}|^2}{M_\#}\,d\xi\,dy\,d\tau \le C\kappa T\,\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr). \label{eq:rescaled-perturbation} \end{align}\qquad{(14)}\] In particular, using the well-preparedness condition 8 , one has \[\begin{align} \int_0^T\iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f^\kappa-\bar f^{\,\kappa}|^2}{M_\#}\,d\xi\,dy\,d\tau \le C\kappa\bigl((\varepsilon_1+\delta_0)^2+\delta_0^{1/2}\bigr)T . \label{eq:rescaled-perturbation-sharp} \end{align}\qquad{(15)}\]
Proof. Let \(t=\tau/\kappa\) and \(x=y/\kappa\). Then \[d\tau\,dy = \kappa^2\,dt\,dx,\] and therefore \[\begin{align} & \int_0^T\int_{\mathbb{R}} \bigl\lVert f^\kappa-\bar f^{\,\kappa}\bigr\rVert_{M_\#}^2 \,dy\,d\tau \\ & \qquad = \kappa^2 \int_0^{T/\kappa}\int_{\mathbb{R}} \bigl\lVert f-\bar f\bigr\rVert_{M_\#}^2\,dx\,dt \\ & \qquad \le \kappa T \sup_{0\le t\le T/\kappa} \int_{\mathbb{R}} \bigl\lVert f-\bar f\bigr\rVert_{M_\#}\,dx \\ &\qquad \le \kappa T \sup_{0\le t\le T/\kappa} \Biggl[\int_{\mathbb{R}} \bigl\lVert M-\bar M\bigr\rVert_{M_\#}^2 \, dx+ \int_{\mathbb{R}} \bigl\lVert\widetilde{G}\bigr\rVert_{M_\#}^2 \, dx \Biggr]\, \qquad \qquad \qquad (\text{by }\eqref{eq:unvar}, \eqref{eq:pevar}) \\ &\qquad \le \kappa T \sup_{0\le t\le T/\kappa} \Biggl[ \bigl\lVert U-\bar U\bigr\rVert_{L^2_x}^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_C\bigr\rVert_{M_\#}^2 \, dx + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{M_\#}^2 \, dx \Biggr] \quad (\text{by } \eqref{eq:mic2}, \eqref{eq:Maxwellian-Lipschitz-single})\\ &\qquad \le C\kappa T\,\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr), \end{align}\] by 107 and ?? . The sharpened bound ?? follows from the well-preparedness hypothesis. ◻
Lemma 11. For each fixed \(T>0\), the families \(\{X_i^\kappa\}_{0<\kappa\le\kappa_0}\), \(i=1,3\), are bounded in \(BV(0,T)\). Consequently, after extraction of a subsequence, there exist \(X_1^0,X_3^0\in BV([0,T])\) such that \[\begin{align} X_i^\kappa \to X_i^0 \qquad\text{in }L^1(0,T), \qquad i=1,3. \label{eq:shift-compactness} \end{align}\qquad{(16)}\] In the rarefaction–contact–shock case, the same conclusion holds for the single family \(\{X_3^\kappa\}\).
Proof. By 52 , \[\frac{d}{d\tau}X_i^\kappa(\tau)=\dot{X}_i\!\left(\frac{\tau}{\kappa}\right),\] hence \[\begin{align} \mathrm{TV}(X_i^\kappa;[0,T]) &= \int_0^T \left|\dot{X}_i\!\left(\frac{\tau}{\kappa}\right)\right|\,d\tau = \kappa\int_0^{T/\kappa} |\dot{X}_i(t)|\,dt \\ &\leq \kappa^{1/2}T^{1/2} \left(\int_0^{T/\kappa}\left| \dot{X}_i\right|^2\right)^{1/2}\leq C_T\delta_i^{-1/2}, \end{align}\] since ?? gives \(\int_0^{T/\kappa}\delta_i|\dot{X}_i|^2 dt\le C\), and \(\delta_i>0\) is fixed. Thus, the family is bounded in \(BV(0,T)\), and the compactness of bounded sets in \(BV(0,T)\) into \(L^1(0,T)\) yields ?? . ◻
Proof of Theorem 2. Let \(f\) be the global normalized solution obtained above, and let \(f^\kappa\) be the rescaled solution 51 . Then \(f^\kappa\) exists uniquely on \([0,T]\) for every \(T>0\), since \(f\) exists globally on \([0,\infty)\).
By Lemma 11, after extraction of a subsequence if necessary, we may assume \[X_i^\kappa \to X_i^0 \qquad\text{in }L^1(0,T), \qquad i=1,3.\]
We first compare \(f^\kappa\) with the rescaled composite approximate wave. By ?? , \[\begin{align} \int_0^T\iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|f^\kappa-\bar f^{\,\kappa}|^2}{M_\#}\,d\xi\,dy\,d\tau \le C\kappa\bigl((\varepsilon_1+\delta_0)^2+\delta_0^{1/2}\bigr)T . \label{eq:main-step-1} \end{align}\tag{53}\]
Next, we compare \(\bar f^{\,\kappa}\) with the shifted Euler Maxwellian profile. Using the exponential localization of the Boltzmann shock profiles(See Lemma 3) and the estimate for the viscous contact wave(See 24 ), we obtain \[\begin{align} \int_0^T\iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|\bar f^{\,\kappa}-M_{X^\kappa}[U^E]|^2}{M_\#} \,d\xi\,dy\,d\tau \le C\delta_C\,\kappa^{1/2}T^{3/2}+ C(\delta_1+\delta_3)\kappa T. \label{eq:main-step-2} \end{align}\tag{54}\]
Finally, by observing that the height of the difference between the two shifted Euler shocks is of order the shock strength, while its width in \(x\) is the difference of the shifts for each shock wave, for each \(\tau\in[0,T]\), \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|M_{X^\kappa}[U^E] - M_{X^0}[U^E]|^2}{M_\#}\,d\xi\,dy \le C\delta_0^2\sum_{i=1,3}|X_i^\kappa(\tau)-X_i^0(\tau)|. \end{align}\] Integrating in \(\tau\) yields \[\begin{align} &\int_0^T\iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|M_{X^\kappa}[U^E] - M_{X^0}[U^E]|^2}{M_\#}\,d\xi\,dy\,d\tau\nonumber\\ &\qquad \le C\delta_0^2\sum_{i=1,3}\|X_i^\kappa-X_i^0\|_{L^1(0,T)}. \label{eq:main-step-3} \end{align}\tag{55}\]
Combining 53 , 54 , and 55 , and using that \(M_\#\) is uniformly bounded from above by positive constants, we obtain \[\begin{align} &\int_0^T \iint_{\mathbb{R}\times\mathbb{R}^3} \left|f^\kappa-M_{X^0}[U^E]\right|^2 \,d\xi\,dy\,d\tau\\ &\quad \le C\kappa\bigl((\varepsilon_1+\delta_0)^2+\delta_0^{1/2}\bigr)T + C\delta_C\,\kappa^{1/2}T^{3/2} + C(\delta_1+\delta_2)\kappa T \\ &\qquad + C\delta_0^2\sum_{i=1,3}\|X_i^\kappa-X_i^0\|_{L^1(0,T)}. \end{align}\] This is exactly ?? . ◻
For simplicity, we introduce the following notation for the left and right end states of the two shock profiles: \[\label{eq:ridx} \begin{align} &v_1:=v_*,\qquad \theta_1:=\theta_*,\qquad p_1:=p_*,\qquad \sigma_{1}^{\text{m}}:=\sigma_*,\\ &v_3:=v^*,\qquad \theta_3:=\theta^*,\qquad p_3:=p^*,\qquad \sigma_{3}^{\text{m}}:=\sigma^*. \end{align}\tag{56}\]
We define \[\label{eq:repy} \Phi(z):=z-1-\ln z,\tag{57}\] and the relative entropy density by \[\label{eq:rel-entropy} \eta(U \mid \bar U) := \frac{2}{3}\bar\theta\,\Phi\!\left(\frac{v}{\bar v}\right) +\bar\theta\,\Phi\!\left(\frac{\theta}{\bar\theta}\right) +\sum_{k=1}^3\frac{\psi_k^2}{2},\tag{58}\] where \[U=(v,u,\theta),\qquad \bar U=(\bar v,\bar u,\bar\theta), \qquad u = (u_1,u_2,u_3), \qquad \bar u = (\bar u_1,0,0).\]
Differentiating 58 with respect to \(t\), we obtain \[\label{eq:etpcom} \begin{align} \partial_t\eta(U \mid \bar U) = \bar\theta_t \left( \frac{2}{3}\Phi\!\left(\frac{v}{\bar v}\right) + \Phi\!\left(\frac{\theta}{\bar\theta}\right) \right) +\sum_{i=1}^3 \psi_i\psi_{it} +\frac{2}{3}\bar\theta \partial_t\Phi\!\left(\frac{v}{\bar v}\right) +\bar\theta \partial_t\Phi\!\left(\frac{\theta}{\bar\theta}\right). \end{align}\tag{59}\]
Substituting the perturbation system 35 –37 into 59 , integrating over \(\mathbb{R}_x\) with the weight \(a(t,x)\), and using the identity \[\frac{\bar p\,\phi}{v}\psi_{1x}+\psi_{1x}(p-\bar p)-\frac{\zeta}{\theta}(pu_{1x}-\bar p\,\bar u_{1x}) = \frac{\bar p\,\phi}{\bar v}\psi_{1x} -\frac{\zeta}{\theta}(p-\bar p)\bar u_{1x},\] together with \[\frac{\bar v\bar p}{v}=\frac{2\bar\theta}{3v}=\frac{\bar\theta p}{\theta},\] we arrive at the weighted relative entropy identity \[\label{eq:weighted-entropy} \frac{d}{dt}\int_{\mathbb{R}} a(t,x)\eta(U \mid \bar U)\,dx = \sum_{i\in\{1,3\}}\dot{X}_i(t)\,\mathcal{Y}_i(U) +\mathcal{J}^{\mathrm{bad}}(U) +\mathcal{J}^{\mathrm{kinetic}}(U) -\mathcal{J}^{\mathrm{good}}(U).\tag{60}\]
Here the modulation functionals are defined by \[\label{eq:Yi} \begin{align} \mathcal{Y}_i(U) &:= -\int_{\mathbb{R}}\partial_x\bigl(a_i^{-X_i}\bigr)\,\eta(U \mid \bar U)\,dx +\int_{\mathbb{R}}a \left( \frac{2}{3}\Phi\!\left(\frac{v}{\bar v}\right) + \Phi\!\left(\frac{\theta}{\bar\theta}\right) \right) \partial_x \bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\,dx\\ &\quad +\int_{\mathbb{R}}a \left( \frac{\partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}}\,\bar p}{\bar v}\phi +\frac{\partial_x \bigl(\theta^{S_{i}}\bigr)^{-X_{i}}}{\bar\theta}\zeta +\psi_1 \partial_x \bigl(u_1^{S_{i}}\bigr)^{-X_{i}} \right)\,dx, \qquad i=1,3. \end{align}\tag{61}\]
We further decompose \[\label{eq:Yi2} \mathcal{Y}_i(U)=\sum_{j=1}^6 \mathcal{Y}_{ij}, \qquad i=1,3\tag{62}\] where \[\label{eq:Yij} \begin{align} &\mathcal{Y}_{i1}:=\int_{\mathbb{R}} a \partial_x(u_1^{S_i})^{-X_i} \psi_1\,dx, \qquad &&\mathcal{Y}_{i2}:=\int_{\mathbb{R}} a \frac{\partial_x\bigl((v^{S_i})^{-X_i}\bigr)\bar p}{\bar v}\phi\,dx, \\ &\mathcal{Y}_{i3}:=\int_{\mathbb{R}} a \frac{\partial_x(\theta^{S_i})^{-X_i}}{\bar\theta}\zeta\,dx, \qquad &&\mathcal{Y}_{i4}:=\frac{2}{3}\int_{\mathbb{R}} a \partial_x \bigl((\theta^{S_i})^{-X_i}\bigr) \Phi\!\left(\frac{v}{\bar v}\right)\,dx, \\ &\mathcal{Y}_{i5}:=\int_{\mathbb{R}} a \partial_x\bigl((\theta^{S_i})^{-X_i}\bigr) \Phi\!\left(\frac{\theta}{\bar\theta}\right)\,dx, \qquad &&\mathcal{Y}_{i6}:=-\int_{\mathbb{R}}\partial_x\bigl(a_i^{-X_i}\bigr)\,\eta(U \mid \bar U)\,dx. \end{align}\tag{63}\]
The good, bad, and kinetic parts in 60 are given by \[\begin{align} \label{eq:good1} \mathcal{J}^{\mathrm{good}}(U) :=& \sum_{i\in\{1,3\}}\sigma_i\int_{\mathbb{R}}\partial_x \bigl(a_i^{-X_i}\bigr)\,\eta(U \mid \bar U)\,dx\nonumber\\ &\quad +\int_{\mathbb{R}} a \left( \frac{\alpha_{\rm{th}}(\bar\theta)}{v\theta}\zeta_x^2 +\frac{4}{3}\frac{\mu(\bar\theta)}{v}\psi_{1x}^2 +\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2 \right)\,dx =:\mathfrak G(U)+\mathcal{D}_{\mathrm{mac}}(U) \end{align}\tag{64}\]
\[\label{eq:bad1} \mathcal{J}^{\mathrm{bad}}(U) := \sum_{\ell=1}^7 \mathcal{B}_\ell(U)+\mathcal{S}_1(U)+\mathcal{S}_2(U),\tag{65}\] and \[\label{eq:kint1} \mathcal{J}^{\mathrm{kinetic}}(U) := \sum_{\ell=1}^6 K_\ell(U).\tag{66}\]
More explicitly, the macroscopic remainder terms are defined by \[\begin{align} &\mathcal{B}_1:=\int_{\mathbb{R}} a\,\mathcal{J}_1\,dx,\\ &\mathcal{J}_1:= \left[\frac{2}{3}\left(-\sigma_1\partial_x\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}+\theta_t^C-\sigma_3\partial_x\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}\right)\Phi\left(\frac{v}{\overline{v}}\right)-\frac{\overline{p}\overline{u}_{1x}}{v\overline{v}}\phi^2\right] \\ &\qquad+\left[\left(-\sigma_1\partial_x\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}+\theta_t^C-\sigma_3\partial_x\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}\right)\Phi\left(\frac{\theta}{\overline{\theta}}\right)-\frac{\overline{u}_{1x}}{\theta}\zeta\left(p-\overline{p}\right)+\overline{p}\overline{u}_{1x}\frac{\zeta^2}{\theta\overline{\theta}}\right]\\ &\qquad =:\mathcal{J}_2+\mathcal{J}_3,\\ &\mathcal{B}_2:=\int_{\mathbb{R}} a_x\,\psi_1(p-\bar p)\,dx,\\ &\mathcal{B}_3:=-\int_{\mathbb{R}}a_x\left[ \frac{\zeta}{\theta}\left(\alpha_{\rm{th}}(\theta)\frac{\theta_x}{v}-\alpha_{\rm{th}}(\bar\theta)\frac{\bar\theta_x}{\bar v}\right) +\frac{4}{3}\psi_1\left(\mu(\theta)\frac{u_{1x}}{v}-\mu(\bar\theta)\frac{\bar u_{1x}}{\bar v}\right)\right.\\ &\left.\qquad \qquad \qquad \qquad +\frac{\mu(\theta)}{v}\sum_{i=2}^3\psi_i\psi_{ix}\right]dx,\\ &\mathcal{B}_4:=\int_{\mathbb{R}} a\,\mathcal{R}_4^{\text{mac}}\,dx,\qquad \mathcal{B}_5:=\int_{\mathbb{R}} a\,\mathcal{R}_5^{\text{mac}}\,dx,\qquad \mathcal{B}_6:=\int_{\mathbb{R}} a\,\mathcal{R}_6^{\text{mac}}\,dx,\\ & \mathcal{S}_1:=-\int_{\mathbb{R}} a\,\psi_1 Q_1\,dx,\qquad \mathcal{S}_2:=-\int_{\mathbb{R}} a\,\frac{\zeta}{\bar\theta}Q_2\,dx, \end{align}\] where \[\begin{align} & \mathcal{R}_4^{\text{mac}} := \biggl[\frac{4}{3}\frac{\mu\bigl(\overline{\theta}\bigr)}{v\overline{v}}\overline{u}_{1x}\psi_{1x}\phi+\frac{\alpha_{\rm{th}}\bigl(\overline{\theta}\bigr)}{\theta^2}\zeta\theta_x\left(\frac{\theta_x}{v}-\frac{\overline{\theta}_x}{\overline{v}}\right)+\frac{\alpha_{\rm{th}}\bigl(\overline{\theta}\bigr)}{v\overline{v}\overline{\theta}}\overline{\theta}_x\zeta_x\phi\biggr.\\ &\biggl.\qquad \qquad \qquad \qquad +\frac{4}{3}\frac{\zeta}{\theta}\left(\mu(\theta)\frac{u_{1x}^2}{v}-\mu\bigl(\overline{\theta}\bigr)\frac{\overline{u}_{1x}^2}{\overline{v}}\right)+\frac{\mu(\theta)}{v}\sum_{i=2}^3 \psi_{ix}^2\biggr], \\ &\mathcal{R}_5^{\text{mac}} := \left[-\frac{\zeta^2}{\theta\overline{\theta}}\left\{\left(\alpha_{\rm{th}}\bigl(\overline{\theta}\bigr)\frac{\overline{\theta}_x}{\overline{v}}\right)_x+\frac{4}{3}\mu\left(\overline{\theta}\right)\frac{\overline{u}_{1x}^2}{v}\right\}\right], \,\\ &\mathcal{R}_6^{\text{mac}} := \left[-\left(\frac{\zeta}{\theta}\right)_x\frac{\theta_x}{v}\left(\alpha_{\rm{th}}(\theta)-\alpha_{\rm{th}}\bigl(\overline{\theta}\bigr)\right)-\frac{4}{3}\frac{u_{1x}\psi_{1x}}{v}\left(\mu(\theta)-\mu\bigl(\overline{\theta}\bigr)\right)\right] \end{align}\]
while the kinetic terms are \[\begin{align} K_1&:=-\iint a\frac{\zeta}{\theta}\left(\xi_1\frac{|\xi|^2}{2}\right)\Bigl(\Pi_1-(\Pi_1^{S_1})^{-X_1}-(\Pi_1^{S_3})^{-X_3}\Bigr)_x\,d\xi\,dx,\\ K_2&:=\iint a\frac{\zeta}{\theta} \left[ u_1\xi_1^2\Pi_{1x} -\sum_{i\in\{1,3\}}(u_1^{S_i})^{-X_i}\xi_1^2\partial_x(\Pi_1^{S_i})^{-X_i} \right]d\xi\,dx,\\ K_3&:=\iint a\frac{\zeta}{\theta}\sum_{i=2}^3\psi_i\,\xi_1\xi_i\,\Pi_{1x}\,d\xi\,dx,\\ K_4&:=-\iint a\psi_1\,\xi_1^2\Bigl(\Pi_1-(\Pi_1^{S_1})^{-X_1}-(\Pi_1^{S_3})^{-X_3}\Bigr)_x\,d\xi\,dx,\\ K_5&:=-\iint a\sum_{i=2}^3\psi_i\,\xi_1\xi_i\,\Pi_{1x}\,d\xi\,dx,\\ K_6&:=\iint a\frac{\zeta^2}{\theta\bar\theta} \sum_{i\in\{1,3\}} \xi_1\left(\frac{|\xi|^2}{2}-(u_1^{S_i})^{-X_i}\xi_1\right)(\partial_x\Pi_1^{S_i})^{-X_i}\,d\xi\,dx. \end{align}\]
The detailed analysis of the leading shock terms, the macroscopic remainders, the kinetic contributions, and the coercive part of \(\mathcal{J}^{\mathrm{good}}\) will be carried out in the following subsections.
We now isolate the leading shock contributions contained in the bad part of the weighted relative entropy identity \(\mathcal{B}_1\). First, we focus on \(\mathcal{J}_2\). Remind \[\label{eq:J2-def} \mathcal{J}_2 = \frac{2}{3}\Bigl(-\sigma_1\partial_x(\theta^{S_1})^{-X_1}+\theta_t^C-\sigma_3\partial_x(\theta^{S_3})^{-X_3}\Bigr) \Phi\!\left(\frac{v}{\bar v}\right) -\frac{\bar p\,\bar u_{1x}}{v\bar v}\phi^2,\tag{67}\] where \[\bar u_{1x} = \partial_x(u_1^{S_1})^{-X_1}+u_{1x}^C+\partial_x(u_1^{S_3})^{-X_3}.\] Accordingly, we split \[\label{eq:J2-split} \mathcal{J}_2=\mathfrak j_{21}+\mathfrak j_{22}+\mathfrak j_{23},\tag{68}\] with \[\begin{align} \mathfrak j_{21} &:= -\frac{2}{3}\sigma_1\partial_x(\theta^{S_1})^{-X_1} \Phi\!\left(\frac{v}{\bar v}\right) -\frac{\bar p\,\partial_x(u_1^{S_1})^{-X_1}}{v\bar v}\phi^2, \tag{69} \\ \mathfrak j_{22} &:= \frac{2}{3}\theta_t^C \Phi\!\left(\frac{v}{\bar v}\right) -\frac{\bar p\,u_{1x}^C}{v\bar v}\phi^2, \tag{70} \\ \mathfrak j_{23} &:= -\frac{2}{3}\sigma_3\partial_x(\theta^{S_3})^{-X_3} \Phi\!\left(\frac{v}{\bar v}\right) -\frac{\bar p\,\partial_x(u_1^{S_3})^{-X_3}}{v\bar v}\phi^2. \tag{71} \end{align}\]
Similarly, we can investigate the term \(\mathcal{J}_3\) as \(\mathcal{J}_2\). Here, \[\label{eq:J3-def} \mathcal{J}_3 = \Bigl(-\sigma_1\partial_x(\theta^{S_1})^{-X_1}+\theta_t^C-\sigma_3\partial_x(\theta^{S_3})^{-X_3}\Bigr) \Phi\!\left(\frac{\theta}{\bar\theta}\right) -\frac{\bar u_{1x}}{\theta}\zeta(p-\bar p) +\bar p\,\bar u_{1x}\frac{\zeta^2}{\theta\bar\theta}.\tag{72}\] We also split \[\label{eq:J3-split} \mathcal{J}_3=\mathfrak j_{31}+\mathfrak j_{32}+\mathfrak j_{33},\tag{73}\] where \[\begin{align} \mathfrak j_{31} &:= -\sigma_1\partial_x(\theta^{S_1})^{-X_1} \Phi\!\left(\frac{\theta}{\bar\theta}\right) -\frac{(p-\bar p)\zeta \partial_x (u_1^{S_1})^{-X_1}}{\theta} +\bar p\,\partial_x (u_1^{S_1})^{-X_1}\frac{\zeta^2}{\theta\bar\theta}, \tag{74} \\ \mathfrak j_{32} &:= \theta_t^C\Phi\!\left(\frac{\theta}{\bar\theta}\right) -\frac{u_{1x}^C}{\theta}\zeta(p-\bar p) +\bar p\,u_{1x}^C\frac{\zeta^2}{\theta\bar\theta}, \tag{75} \\ \mathfrak j_{33} &:= -\sigma_3\partial_x(\theta^{S_3})^{-X_3} \Phi\!\left(\frac{\theta}{\bar\theta}\right) -\frac{(p-\bar p)\zeta \partial_x(u_1^{S_3})^{-X_3}}{\theta} +\bar p\,\partial_x (u_1^{S_3})^{-X_3}\frac{\zeta^2}{\theta\bar\theta}. \tag{76} \end{align}\]
We use Taylor expansions \[\label{eq:taylor-Phi} \Phi\!\left(\frac{v}{\bar v}\right) = \frac{\phi^2}{2\bar v^2}+O(|\phi|^3), \qquad \Phi\!\left(\frac{\theta}{\bar\theta}\right) = \frac{\zeta^2}{2\bar\theta^2}+O(|\zeta|^3),\tag{77}\] together with 22 and Lemma 1 \[\label{eq:thetaC-t} \theta_t^C = -p^C u_{1x}^C +\left(\frac{\alpha_{\rm{th}}(\theta^C)\theta_x^C}{v^C}\right)_x +\frac{4}{3}\mu(\theta^C)\frac{(u_{1x}^C)^2}{v^C} +Q_2^C,\tag{78}\] where \[\label{eq:Q2C-bound} Q_2^C = O(1)\delta_C(1+t)^{-2}e^{-2c_0x^2/(1+t)}.\tag{79}\] Moreover, see (4.35) in [37], by Lemma 3, \[\label{eq:pbar-endstate} |\bar p- p_1|+|\bar p- p_3|\le C\delta_0.\tag{80}\]
The next estimates follow from 77 –80 , the exponential localization of the shock profiles, and the Gaussian estimate for the viscous contact wave. See (4.33) with \(\gamma=\frac{5}{3}\) in [37]: \[\begin{align} \mathfrak j_{21} &\le -\frac{4 p_1\,\sigma_1^{\text{m}}}{3 v_1^2}\partial_x(v^{S_1})^{-X_1}\phi^2 + C(\delta_0+\varepsilon)|\partial_x(v^{S_1})^{-X_1}|\phi^2, \tag{81} \\ \mathfrak j_{22} &\le C\delta_C(1+t)^{-1}e^{-C_1|x|^2/(1+t)}\phi^2, \tag{82} \\ \mathfrak j_{23} &\le \frac{4p_3\,\sigma_3^{\text{m}}}{3 v_3^2}\partial_x(v^{S_3})^{-X_3}\phi^2 + C(\delta_0+\varepsilon)|\partial_x(v^{S_3})^{-X_3}|\phi^2. \tag{83} \end{align}\] Similarly, \[\begin{align} \label{eq:J3-est} \mathcal{J}_3 \le& \sum_{i\in\{1,3\}} \frac{\sigma_i^{\text{m}} |\partial_x(v^{S_i})^{-X_i}|}{2v_i\theta_i} \left(\frac{2}{3}\zeta-2p_i\phi \right) \zeta + C\delta_C(1+t)^{-1}e^{-C_1|x|^2/(1+t)}|(\phi,\zeta)|^2 \nonumber \\ &\qquad+ C(\delta_0+\varepsilon)\bigl(|\partial_x(v^{S_1})^{-X_1}|+|\partial_x(v^{S_3})^{-X_3}|\bigr)|(\phi,\zeta)|^2. \end{align}\tag{84}\]
Consequently, we obtain the following estimate for the leading shock contribution: \[\label{eq:nbad1} \begin{align} \int_{\mathbb{R}}a(\mathcal{J}_2+\mathcal{J}_3)\,dx \le\;& \sum_{i=1,3}\int_{\mathbb{R}}a\,|\partial_x(v^{S_i})^{-X_i}| \left( \frac{4p_i\sigma_i^{\text{m}}}{3v_i^2}\phi^2 +\frac{\sigma_i^{\text{m}}}{3v_i\theta_i}\zeta^2 -\frac{p_i\sigma_i^{\text{m}}}{v_i\theta_i}\phi\zeta \right)\,dx\\ &+ C\delta_C(1+t)^{-1}\int_{\mathbb{R}}ae^{-C_1|x|^2/(1+t)}|(\phi,\zeta)|^2\,dx\\ &+ C(\delta_0+\varepsilon)\int_{\mathbb{R}} \bigl(|\partial_x(v^{S_1})^{-X_1}|+|\partial_x(v^{S_3})^{-X_3}|\bigr)|(\phi,\zeta)|^2\,dx. \end{align}\tag{85}\] The remaining dominant terms are estimated in the following lemma by using the a-contraction method.
We now rewrite the weighted relative entropy identity 60 by using 85 . More precisely, we decompose the right-hand side into modulation terms, macroscopic error terms, microscopic error terms, and coercive contributions: \[\label{eq:energy2} \begin{align} &\frac{d}{dt}\int_{\mathbb{R}}a\,\eta(U\mid\bar U)\,dx \\ &\quad \le \sum_{i\in\{1,3\}}\dot{X}_i(t)\mathcal{Y}_i(U) +\mathcal{B}^{\text{sh}} + \sum_{l=2}^6 \mathcal{B}_l + \mathcal{B}^{\text{res}} +\mathcal{S}_1+\mathcal{S}_2 +\sum_{l=1}^6 K_l -\mathfrak G(U)-\mathcal{D}_{\mathrm{mac}}(U). \end{align}\tag{86}\] Here, the reformulated error terms \(\mathcal{B}^{\text{sh}}, \, \mathcal{B}^{\text{res}}\) are defined by \[\begin{align} & \mathcal{B}^{\text{sh}}:=\sum_{i\in\{1,3\}}\int_{\mathbb{R}}a|\partial_x(v^{S_i})^{-X_i}| \left( \frac{4p_i\sigma_{i}^{\text{m}}}{3v_i^2}\phi^2 +\frac{\sigma_{i}^{\text{m}}}{3v_i\theta_i}\zeta^2 -\frac{p_i\sigma_{i}^{\text{m}}}{v_i\theta_i}\phi\zeta \right)\,dx, \\ & \mathcal{B}^{\text{res}}:=C\delta_C\frac{1}{1+t}\int_{\mathbb{R}}ae^{-C_1|x|^2/(1+t)}|(\phi,\zeta)|^2\,dx \\ &\qquad \qquad+C(\delta_0+\varepsilon)\int_{\mathbb{R}}\bigl(|\partial_x(v^{S_1})^{-X_1}|+|\partial_x(v^{S_3})^{-X_3}|\bigr)|(\phi,\zeta)|^2\,dx. \end{align}\]
Lemma 12. For \(t>0\), there exist positive constants \(C\) and \(\alpha\) such that \[\begin{align} \label{eq:macro1} & -\sum_{i=1,3}\frac{\delta_i}{2M_i}|\dot{X}_i|^2 + \mathcal{B}^{\mathrm{sh}} + \mathcal{B}_2 - \mathfrak G - \frac{3}{4} \mathcal{D}_{\mathrm{mac}} \\ & \quad \le\; -\alpha\sum_{i=1,3}\mathcal{G}_i^S+C\delta_1^{\frac{4}{3}}\bigl(\delta_3^{\frac{4}{3}}+\delta_C^{\frac{4}{3}}\bigr)e^{-C\delta_1 t} + C\delta_3^{\frac{4}{3}}\bigl(\delta_1^{\frac{4}{3}}+\delta_C^{\frac{4}{3}}\bigr)e^{-C\delta_3 t}\nonumber\\ & \qquad + C\left(\sum_{i=1,3}\delta_i^2e^{-C\delta_i t}+\frac{1}{\delta_*t^2}\right)\int_{\mathbb{R}}\eta(U \mid \bar U)\,dx - \frac{3}{4}\int_{\mathbb{R}}a\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2\,dx. \end{align}\qquad{(17)}\] Recall that \[\label{eq:maccoreciv} \mathcal{G}_i^S := \int_{\mathbb{R}}\Bigl|\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr|\,|\varphi_i(\phi,\psi,\zeta)|^2\,dx.\qquad{(18)}\]
Proof. We next combine the modulation terms, the principal shock contribution \(\mathcal{B}^{\text{sh}}\), and the dissipative part \(\mathcal{D}_{\mathrm{mac}}(U)\) in order to recover the coercive shock functional \(\mathcal{G}_i^S\).
See (4.46) with \(R=\frac{2}{3}\) in [37]. By a similar argument, we obtain the following estimate. \[\label{eq:nbad2} \begin{align} \mathcal{B}_2(U)-\mathfrak G(U) \le\;& -\sum_{i\in\{1,3\}}\mathfrak G_{1i}(U) -\sum_{i\in\{1,3\}}\mathfrak G_{2i}(U) -\sum_{i\in\{1,3\}}\mathfrak G_{3i}(U) +B_{\mathrm{new}}(U)\\ &+ C\sum_{i\in\{1,3\}}\delta_i\sqrt{\delta_i}e^{-C\delta_i t} \int_{\mathbb{R}}\eta(U \mid \bar U)\,dx, \end{align}\tag{87}\] where \[\begin{align} \begin{aligned} & \mathfrak G_{1i}(U):=\frac{\theta_i\sigma_{i}^{\text{m}}}{3v_i^2}\int_{\mathbb{R}}|\partial_x(a_i^{-X_i})|\varphi_i\left(\phi+\frac{\psi_1}{\sigma_i^{\text{m}}}\right)^2dx,\\ & \mathfrak G_{2i}(U):=\frac{\sigma_{i}^{\text{m}}}{2\theta_i}\int_{\mathbb{R}}|\partial_x(a_i^{-X_i})|\varphi_i\left(\zeta-\frac{2\theta_i}{3\sigma_i^{\text{m}} v_i}\psi_1\right)^2dx,\\ & \mathfrak G_{3i}(U):=\frac{\sigma_{i}}{2}\sum_{j=2}^3\int_{\mathbb{R}}\partial_x(a_i^{-X_i})\varphi_i \psi_j^2dx=\frac{1}{2\sqrt{\delta_i}}\sum_{j=2}^3\int_\mathbb{R}\sigma_i\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\varphi_i\psi_j^2 dx, \end{aligned} \end{align}\] and \[\begin{align} \begin{aligned} B_{\mathrm{new}}(U):=\;& C\sum_{i\in\{1,3\}}\delta_i\int_{\mathbb{R}}|\partial_x(a_i^{-X_i})||(\phi,\psi,\zeta)|^2dx + C\sum_{i\in\{1,3\}}\int_{\mathbb{R}}|\partial_x(a_i^{-X_i})||(\phi,\psi,\zeta)|^3dx\\ &+ C\int_{\mathbb{R}}|\partial_x(a_1^{-X_1})| \Bigl(|(v^{S_3}-v^*,\theta^{S_3}-\theta^*)|+|(v^C-v_*,\theta^C-\theta_*)|\Bigr) |(\phi,\psi_1,\zeta)|^2dx\\ &+ C\int_{\mathbb{R}}|\partial_x(a_3^{-X_3})| \Bigl(|(v^{S_1}-v_-,\theta^{S_1}-\theta_-)|+|(v^C-v_*,\theta^C-\theta_*)|\Bigr) |(\phi,\psi_1,\zeta)|^2dx. \end{aligned} \end{align}\] Indeed, \[\begin{align} \mathcal{B}_2(U)-\mathfrak G(U) &= \int_{\mathbb{R}} a_x \psi_1(p-\bar p)\,dx -\sum_{i\in\{1,3\}}\sigma_i \int_{\mathbb{R}} \partial_x(a_i^{-X_i}) \eta(U\mid \bar U)\,dx\\ &= \sum_{i\in\{1,3\}} \int_{\mathbb{R}}\partial_x(a_i^{-X_i}) \left[ \psi_1(p-\bar p) -\sigma_i\left( \frac{2}{3}\bar\theta\Phi\!\left(\frac{v}{\bar v}\right) +\bar\theta\Phi\!\left(\frac{\theta}{\bar\theta}\right) +\frac{|\psi|^2}{2} \right) \right]dx. \end{align}\] Using \[\begin{align} \Phi(z)=\frac{(z-1)^2}{2}+O(|z-1|^3), \quad p-\bar p=\frac{2}{3v}\zeta-\frac{\bar p}{v}\phi, \end{align}\] we complete squares separately for the \(1\)-shock and \(3\)-shock contributions and obtain 87 . Here, the good terms \(\mathfrak G_{3i}\) are the coercivity of the transverse velocities included in \(\mathcal{G}_i^S\).
It remains to estimate \(B_{\mathrm{new}}\). Using \(\varphi_1+\varphi_3=1\), Lemmas 3–6, the Sobolev inequality, and Young’s inequality, we obtain
\[\begin{align} \begin{aligned} B_{\mathrm{new}}(U)\le\;& C(\varepsilon+\sqrt{\delta_0}) \left( \sum_{i\in\{1,3\}}(\mathfrak G_{1i}+\mathfrak G_{2i})+\mathcal{D}_{\mathrm{mac}}(U)+\sum_{i=1,3}\mathcal{G}_i^S \right)\\ &+ C\sum_{i\in\{1,3\}}\varepsilon\sqrt{\delta_i}\delta_i e^{-C\delta_i t} \int_{\mathbb{R}}\eta(U \mid \bar U)\,dx\\ &+ C\delta_1^{\frac{4}{3}}\bigl(\delta_C^{\frac{4}{3}}+\delta_3^{\frac{4}{3}}\bigr)e^{-C\delta_1t}+ C\delta_3^{\frac{4}{3}}\bigl(\delta_C^{\frac{4}{3}}+\delta_1^{\frac{4}{3}}\bigr)e^{-C\delta_3t}. \end{aligned} \end{align}\]
We now estimate the modulation term \[-\sum_{i=1,3}\frac{\delta_i}{2\mathfrak m_i}|\dot{X}_i|^2.\] Set \[\label{eq:newvar} \begin{align} & w_1:=\varphi_1\psi_1,\qquad w_3:=\varphi_3\psi_1,\\ & y_1:= -\frac{\left(v^{S_1}\right)^{-X_1}-v_-}{\delta_1},\qquad y_3:= \frac{\left(v^{S_3}\right)^{-X_3}-v^*}{\delta_3},\\ & z_1:=x-\sigma_1 t-X_1(t),\qquad z_3:=x-\sigma_3 t-X_3(t), \end{align}\tag{88}\] so that \[\frac{dy_1}{dz_1}=-\frac{\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}}{\delta_1}>0, \qquad \frac{dy_3}{dz_3}=\frac{\partial_x\bigl(v^{S_{3}}\bigr)^{-X_{3}}}{\delta_3}>0.\]
Using the decomposition \(\mathcal{Y}_i=\sum_{j=1}^6\mathcal{Y}_{ij}\), we write the shift ODE in the form \[\label{eq:dsaf} \dot{X}_i(t)=-\frac{\mathfrak m_i}{\delta_i}(\mathcal{Y}_{i1}+\mathcal{Y}_{i2}+\mathcal{Y}_{i3}), \qquad i=1,3.\tag{89}\] For the \(1\)-shock, the terms \(\mathcal{Y}_{11},\mathcal{Y}_{12},\mathcal{Y}_{13}\) can be compared with \(\int_0^1 w_1\,dy_1\). More precisely, \[\begin{align} \left|\mathcal{Y}_{11}+\delta_1\sigma_{1}^{\text{m}}\int_0^1w_1\,dy_1\right| &\le C\delta_1(\sqrt{\delta_0}+\delta_0)\int_0^1|w_1|\,dy_1 \nonumber \\ &\quad + C\int_{\mathbb{R}}|\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}|\varphi_3|\psi_1|\,dx, \\ \left|\mathcal{Y}_{12}+\frac{p_1\delta_1}{\sigma_{1}^{\text{m}}v_1}\int_0^1w_1\,dy_1\right| &\le C\delta_1(\delta_0+\sqrt{\delta_0})\int_0^1|w_1|\,dy_1 \nonumber\\ &\quad + C\sqrt{\delta_1}\int_{\mathbb{R}}|\partial_x(a_1^{-X_1})|\varphi_1\left|\phi-\frac{\psi_1}{\sigma_1}\right|dx \nonumber \\ &\quad + C\int_{\mathbb{R}}\left|\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|\varphi_3|\phi|\,dx, \\ \left|\mathcal{Y}_{13}+\frac{2}{3}\frac{p_1\delta_1}{\sigma_{1}^{\text{m}}v_1}\int_0^1w_1\,dy_1\right| &\le C\delta_1(\delta_0+\sqrt{\delta_0}+\varepsilon)\int_0^1|w_1|\,dy_1 \nonumber\\ &\quad + C\sqrt{\delta_1}\int_{\mathbb{R}}|\partial_x(a_1^{-X_1})|\varphi_1\left|\zeta-\frac{2\theta_-}{3\sigma_1v_-}\psi_1\right|dx\nonumber\\ &\quad + C\int_{\mathbb{R}}\varphi_3\left|\partial_x\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\right||\zeta|\,dx. \end{align}\] Hence, \[\begin{align} \left|\dot{X}_1-2\sigma_1^{\text{m}}\mathfrak m_1\int_0^1w_1\,dy_1\right|^2 \le\;& C(\delta_0+\sqrt{\delta_0}+\varepsilon)^2\int_0^1 w_1^2\,dy_1 +\frac{C}{\delta_1}(\mathfrak G_{11}+\mathfrak G_{21}) \nonumber\\ &+C\delta_1e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U \mid \bar U)\,dx. \end{align}\] Therefore, \[\begin{align} -\frac{\delta_1}{2\mathfrak m_1}|\dot{X}_1|^2 \le\;& -(\sigma_1^{\text{m}})^2\mathfrak m_1\delta_1\left(\int_0^1 w_1\,dy_1\right)^2 + C\delta_1(\delta_0+\sqrt{\delta_0}+\varepsilon)^2\int_0^1w_1^2\,dy_1 \\ &+ C\sqrt{\delta_1}(\mathfrak G_{11}+\mathfrak G_{21}) + C\delta_1^2e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx. \end{align}\] The \(3\)-shock case is treated in the same way.
Recall that \[\mathcal{B}^{\text{sh}}(U) = \sum_{i\in\{1,3\}} \int_{\mathbb{R}} a\Bigl|\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr| \left( \frac{4p_i\sigma_{i}^{\text{m}}}{3v_i^2}\phi^2 +\frac{\sigma_{i}^{\text{m}}}{3v_i\theta_i}\zeta^2 -\frac{\sigma_{i}^{\text{m}} p_i}{v_i\theta_i}\phi\zeta \right)\,dx.\] We decompose \[\mathcal{B}_1=\sum_{i\in\{1,3\}}(B_{11}^i+B_{12}^i+B_{13}^i)\] according to the three terms inside the bracket. By splitting \(\phi\) and \(\zeta\) into the favorable part on \(\varphi_i\) and the exponentially small interaction part on \(1-\varphi_i^2\), and using Lemma 6, we obtain \[\begin{align} B_{11}^1 &\le \frac{4p_1}{3v_1^2\sigma_{1}^{\text{m}}}(1+\sqrt{\delta_0}+\delta_1^{1/4})\delta_1\int_0^1|w_1|^2\,dy_1 \nonumber\\ &\quad + C\delta_1^{1/4}\mathfrak G_{11} + C\delta_1^2e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx, \\ B_{12}^1 &\le \frac{p_1}{3\sigma_{1}^{\text{m}}v_1^2}(1+\sqrt{\delta_0}+\delta_1^{1/4})\delta_1\int_0^1|w_1|^2\,dy_1 \nonumber\\ &\quad + C\delta_1^{1/4}\mathfrak G_{21} + C\delta_1^2e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx, \\ B_{13}^1 &\le \frac{\sigma_{1}^{\text{m}}p_1}{v_1\theta_1}(1+\sqrt{\delta_0}+\delta_1^{1/4})\delta_1\int_0^1|w_1|^2\,dy_1 \nonumber\\ &\quad + C\delta_1^{1/4}(\mathfrak G_{11}+\mathfrak G_{21}) + C\delta_1^2e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx. \end{align}\] The same estimate holds for the \(3\)-shock contribution. Consequently, \[\begin{align} \mathcal{B}^{\text{sh}} \le\;& \sum_{i\in\{1,3\}} \frac{20p_i}{9v_i^2\sigma_{i}^{\text{m}}}(1+\sqrt{\delta_0}+\delta_i^{1/4}) \delta_i\int_0^1|w_i|^2\,dy_i \\ &+ C\sum_{i\in\{1,3\}}\delta_i^{1/4}(\mathfrak G_{1i}+\mathfrak G_{2i}) + C\sum_{i\in\{1,3\}}\delta_i^2e^{-C\delta_i t} \int_{\mathbb{R}}\eta(U \mid \bar U)\,dx. \end{align}\]
Recall that \[\mathcal{D}_{\mathrm{mac}}(U) = \int_{\mathbb{R}}a \left( \frac{\alpha_{\rm{th}}(\bar\theta)}{v\theta}\zeta_x^2 + \frac{4}{3}\frac{\mu(\bar\theta)}{v}\psi_{1x}^2 + \frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2 \right)dx.\] Using the cutoff decomposition and the change of variable \(x\mapsto y_i\), together with Lemmas 4 and 5, we obtain \[\begin{align}\label{eq:diffusion} -\mathcal{D}_{\mathrm{mac}}(U) \le\;& -\sum_{i\in\{1,3\}}2\alpha_i\bigl(1-C(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*)-\delta_i^{1/4}\bigr)\delta_i\int_0^1 w_i^2\,dy_i \\ &+ \sum_{i\in\{1,3\}}\frac{20+12\gamma}{10+3\gamma}\alpha_i\delta_i\bigl( w_i^{\mathrm{avg}}\bigr)^2 + \sum_{i\in\{1,3\}}C\delta_i^{1/4}\mathfrak G_{2i} \\ &+ \frac{C}{\delta_*t^2}\int_{\mathbb{R}}\eta(U|\bar U)\,dx - \int_{\mathbb{R}}a\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2\,dx, \end{align}\tag{90}\] where \[\alpha_i=\frac{20}{9}\frac{p_i}{\sigma_{i}^{\text{m}} v_i^2}, \qquad w_i^{\mathrm{avg}}:=\int_0^1 w_i\,dy_i, \qquad \gamma=\frac{\alpha_{\rm{th}}(\bar\theta)}{\mu(\bar\theta)}.\]
More precisely, to investigate the diffusion term, we decompose as follows. \[\begin{align} \begin{aligned} \widetilde{D}_{u_1}(U)=\int_\mathbb{R} a \left(\frac{4}{3}\frac{\mu(\overline{\theta})}{v}\psi_{1x}^2\right)dx,\quad \widetilde{D}_{\theta}(U)=\int_\mathbb{R} a \left(\frac{\alpha_{\rm{th}}(\overline{\theta})}{v\theta}\zeta_x^2\right)dx. \end{aligned} \end{align}\]
We focus on \(\widetilde{D}_{u_1}\). Observe that
\[\begin{align} \begin{aligned} \widetilde{D}_{u_1}(U)\geq \sum_{i\in\{1,3\}}\int_\mathbb{R} a \varphi_i^2 \frac{4}{3}\frac{\mu(\overline{\theta})}{v}\psi_{1x}^2dx. \end{aligned} \end{align}\]
Using the Young inequality, we have the following.
\[\begin{align} \begin{aligned} \int_\mathbb{R} a \frac{\mu(\overline{\theta})}{v}\left| \left(\varphi_i \psi_1\right)_x\right|^2dx\leq (1+\delta_*)\int_\mathbb{R} a\frac{\mu(\overline{\theta})}{v}\varphi_i^2\psi_{1x}^2dx+\frac{C}{\delta_*}\int_\mathbb{R} a \frac{\mu(\overline{\theta})}{v}\left| \varphi_{ix}\right|^2\left| \psi_1\right|^2dx \end{aligned} \end{align}\]
for any sufficiently small \(\delta_*>0\) that is chosen later.
Since \(\varphi_1^2+\varphi_3^2\leq 1\), we get the following estimate,
\[\begin{align} \begin{aligned} -\widetilde{D}_{u_1}(U)\leq -\frac{1}{1+\delta_*}\frac{4}{3}\sum_{i\in\{1,3\}}\int_\mathbb{R} a \frac{\mu(\overline{\theta})}{v}\left| \left(\varphi_i\psi_1\right)_x\right|^2dx+\frac{4}{3}\frac{C}{\delta_*}\int_\mathbb{R} a\frac{\mu(\overline{\theta})}{v}\left(\varphi_{ix}\right)^2\left| \psi_1\right|^2dx. \end{aligned} \end{align}\]
For clarity, each term is defined as follows.
\[\begin{align} \begin{aligned} &J_1 := -\frac{1}{1+\delta_*}\sum_{i\in\{1,3\}}\int_\mathbb{R} a \frac{\mu(\overline{\theta})}{v}\left| \left(\varphi_i\psi_1\right)_x\right|^2dx,\\ &J_2:= \frac{C}{\delta_*}\int_\mathbb{R} a\frac{\mu(\overline{\theta})}{v}\left(\varphi_{ix}\right)^2\left| \psi_1\right|^2dx. \end{aligned} \end{align}\]
By the change of variable(cf. 88 ), we have
\[\begin{align} \begin{aligned} J_1 = -\frac{1}{1+\delta_*}\sum_{i\in\{1,3\}}\int_0^1 a \frac{\mu(\overline{\theta})}{v}\frac{dy_i}{dx}\left| (w_i)_{y_i}\right|^2dy_i. \end{aligned} \end{align}\]
From Lemmas 4 and 5, we have the following. \[\begin{align} \begin{aligned} \frac{dy_1}{dz_1}\geq \Biggl(\frac{1}{y_1(1-y_1)}\frac{4}{3}\frac{\mu\Bigl(\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\Bigr)}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}}\Biggr)^{-1}(A\alpha_1\delta_1-C\delta_1^2)>0 \end{aligned} \end{align}\] where \(A := \frac{10}{10+\gamma}\).
Therefore, we can get the following estimate, \[\begin{align} \begin{aligned} J_1&\leq -\frac{1}{1+\delta_*}\sum_{i\in\{1,3\}}\int_0^1 a \frac{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}{v}\frac{\mu(\overline{\theta})}{\mu\left(\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\right)}\frac{3}{4}y_i(1-y_i)(A\alpha_i\delta_i-C\delta_i^2)\left| \left(w_i\right)_{y_i}\right|^2dy_i\\ &\leq -\frac{1}{1+\delta_*}\sum_{i\in\{1,3\}}\int_0^1 \frac{3}{4}(1-2\sqrt{\delta_0})(1-C\varepsilon)(A\alpha_i-C\delta_i)\delta_iy_i(1-y_i)\left| \left(w_i\right)_{y_i}\right|^2dy_i. \end{aligned} \end{align}\] Since \(\frac{1}{1+\delta_*}\geq 1-\delta_*\) and \[\begin{align} \begin{aligned} (1-2\sqrt{\delta_0})(1-C\varepsilon)(A\alpha_i-C\delta_i)(1-\delta_*)\geq A\alpha_i(1-C(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*)), \end{aligned} \end{align}\]
we organize the above estimate as follows.
\[\begin{align} \begin{aligned} J_1\leq -\sum_{i\in\{1,3\}}\int_0^1 \frac{3}{4}A\alpha_i(1-C(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*))\delta_iy_i(1-y_i)\left| \left(w_i\right)_{y_i}\right|^2dy_i. \end{aligned} \end{align}\]
Now, we consider another term which is singular at time \(t=0\). By 46 , \[\frac{1}{2}\left(X_3(t)+\sigma_3t-X_1(t)-\sigma_1t\right)\geq \frac{\sigma_3-\sigma_1}{4}t>0, \quad T\geq t>0\] we have \[\begin{align} \begin{aligned}\label{eq:cutof1} &\left| \varphi_{ix}\right|\leq \frac{4}{\sigma_3-\sigma_1}\frac{1}{t},\quad \left| \varphi_{ix}\right|^2\leq \frac{16}{(\sigma_3-\sigma_1)^2}\frac{1}{t^2}, \quad T\geq t>0, \quad \forall x\in \mathbb{R}. \end{aligned} \end{align}\tag{91}\] From this, we can compute \[\begin{align} \begin{aligned} &J_2=\frac{C}{\delta_*}\int_\mathbb{R} a \frac{\mu(\overline{\theta})}{v}\left| \varphi_{ix}\right|^2\left| \psi_1\right|^2dx\leq \frac{C}{\delta_*t^2}\int_\mathbb{R} \eta(U\mid\bar{U})dx. \end{aligned} \end{align}\] Thus, we have the estimate of \(\widetilde{D}_{u_1}\) as follows: \[\begin{align} \begin{aligned} &-\widetilde{D}_{u_1}\leq-\sum_{i\in\{1,3\}}\int_0^1\frac{3}{4}A\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*\right)\right)\delta_iy_i(1-y_i)\left| \left(w_i\right)_{y_i}\right|^2dy_i\\ &\qquad \qquad \qquad +\frac{C}{\delta_*t^2}\int_\mathbb{R}\eta(U\mid\bar{U})dx. \end{aligned} \end{align}\]
By the same manner, we perform the same procedure to \(\widetilde{D}_{\theta_1}(U)\). Take \(\mathfrak z_i = \varphi_i \zeta\) for \(i=1,3\). Then, we have the following estimate.
\[\begin{align} \begin{aligned}\label{eq:diffusionx} -\mathcal{D}_{\mathrm{mac}}(U)\leq&-\sum_{i\in\{1,3\}}\int_0^1A\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*\right)\right)\delta_iy_i(1-y_i)\left| \left(w_i\right)_{y_i}\right|^2dy_i\\ &-\sum_{i\in\{1,3\}}\int_0^1\frac{3}{4}A\alpha_i\frac{\gamma}{\theta_i}\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*\right)\right)\delta_iy_i(1-y_i)\left| \left(\mathfrak z_i\right)_{y_i}\right|^2dy_i\\ & +\frac{C}{\delta_*t^2}\int_\mathbb{R}\eta(U\mid\bar{U})dx-\int_\mathbb{R} a \left(\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2\right)dx. \end{aligned} \end{align}\tag{92}\]
Now, to replace \(\mathfrak z_i\) by \(w_i\), we compute these as follows.
\[\begin{align} \begin{aligned} &\int_0^1 \left| \mathfrak z_i\right|^2 dy_i \geq \left(\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\right)^2\left(1-\delta_i^{\frac{1}{4}}\right)\int_0^1 \left| w_i\right|^2 dy_i-\frac{C}{\delta_i^{\frac{1}{4}}}\int_0^1 \left[\varphi_i\left(\zeta-\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\psi_{1}\right)\right]^2dy_i,\\ &\left(\int_0^1 \mathfrak z_i dy_i\right)^2\leq 2\left[\int_0^1 \frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\varphi_i\psi_{1}dy_i\right]^2+2\left[\int_0^1 \varphi_i\left(\zeta-\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\varphi_i\psi_{1}\right)dy_i\right]^2. \end{aligned} \end{align}\] Now, we introduce the following useful lemma for estimating 92 .
Lemma 13 ([31]). For any \(f:[0,1]\rightarrow \mathbb{R}\) satisfying \(\int_0^1 y(1-y)\left| f'\right|^2 dy<\infty\), \[\label{eq:poincare} \int_0^1 \left| f-\int_0^1 f dy\right|^2 dy \leq \frac{1}{2} \int_0^1 y(1-y)\left| f'\right|^2 dy.\qquad{(19)}\]
By the Poincare inequality ?? , we have \[\begin{align} \begin{aligned} &-\mathcal{D}_{\mathrm{mac}}(U)\\ &\quad \le -\sum_{i\in\{1,3\}}2A\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*\right)\right)\delta_i\left[\int_0^1 w_i^2 dy_i-\bigl(w_i^{\mathrm{avg}}\bigr)^2\right]\\ &\quad \quad-\sum_{i\in\{1,3\}}\frac{3}{4}2A\alpha_i\frac{\gamma}{\theta_i}\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_i+\delta_*\right)\right)\delta_i\left[\int_0^1z_i^2 dy_i-\bigl(z_i^{\mathrm{avg}}\bigr)^2\right]\\ &\quad \quad+\frac{C}{\delta_*t^2}\int_\mathbb{R}\eta(U\mid\bar{U})dx-\int_\mathbb{R} a \left(\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2\right)dx \\ &\quad \le -\sum_{i\in\{1,3\}}2A\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)\right)\delta_i\left\{1+\frac{3}{4}\frac{\gamma}{\theta_i}\left(\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\right)^2\left(1-\delta_i^{\frac{1}{4}}\right)\right\}\int_0^1 w_i^2 dy_i\\ &\quad \quad +\sum_{i\in\{1,3\}}2A\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)\right)\delta_i\left\{1+\frac{3}{4}2\frac{\gamma}{\theta_i}\left(\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\right)^2\right\}\bigl(w_i^{\mathrm{avg}}\bigr)^2\\ &\quad \quad +\sum_{i\in\{1,3\}}\frac{3}{2}A\alpha_i\frac{\gamma}{\theta_i}\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)\right)\delta_i\left(\frac{C}{\delta_i^{\frac{1}{4}}}-2\right)\int_0^1 \left[\varphi_i\left(\zeta-\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\psi_{1i}\right)\right]^2 dy_i\\ &\quad \quad +\frac{C}{\delta_*t^2}\int_\mathbb{R}\eta(U\mid\bar{U})dx-\int_\mathbb{R} a \left(\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2\right)dx. \end{aligned} \end{align}\] Also, we control the third term of right hand side of the above inequality as followed: \[\begin{align} \begin{aligned} & \sum_{i\in\{1,3\}}\frac{3}{2}A\alpha_i\frac{\gamma}{\theta_i}\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)\right)\delta_i\left(\frac{C}{\delta_i^{\frac{1}{4}}}-2\right)\int_0^1 \left[\varphi_i\left(\zeta-\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\psi_{1}\right)\right]^2 dy_i \\ & \le \sum_{i\in\{1,3\}}\frac{3}{2}CA\alpha_i\frac{\gamma}{\theta_i}\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)\right)\delta_i^{\frac{3}{4}}\int_0^1\varphi_i \left[\left(\zeta-\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\psi_{1}\right)\right]^2 dy_i\\ & \le \sum_{i\in\{1,3\}}C\delta_i^{\frac{1}{4}}\mathfrak G_{2i}. \end{aligned} \end{align}\] We organize the first term of right hand side of the above inequality as followed: \[\begin{align} \begin{aligned} &-\sum_{i\in\{1,3\}}2A\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)-\delta_i^{\frac{1}{4}}\right)\delta_i\left\{1+\frac{3}{4}\frac{\gamma}{\theta_i}\left(\frac{2\theta_i}{3\sigma_i^{\text{m}}v_i}\right)^2\right\}\int_0^1 w_i^2 dy_i\\ \le&-\sum_{i\in\{1,3\}}2\alpha_i\left(1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)-\delta_i^{\frac{1}{4}}\right)\delta_i\int_0^1 w_i^2 dy_i. \end{aligned} \end{align}\]
Therefore, we have \[\begin{align} \begin{aligned} & \sum_{i\in\{1,3\}}2A\alpha_i\left(1-C\left(\sqrt{\delta}+\varepsilon+\delta_*\right)\right)\delta_i\left\{1+\frac{3}{2}\frac{\gamma}{\theta_i}\left(\frac{2\theta_i}{3\sigma_iv_i}\right)^2\right\}\bigl(w_i^{\mathrm{avg}}\bigr)^2\\ \leq & \sum_{i\in\{1,3\}}\frac{20+12\gamma}{10+3\gamma} \alpha_i\delta_i\bigl(w_i^{\mathrm{avg}}\bigr)^2. \end{aligned} \end{align}\]
Then, we obtained the estimate 90 .
Choose \(\delta_*=O(1)>0\) such that \[\begin{align} 1-C\left(\sqrt{\delta_0}+\varepsilon+\delta_*\right)-\delta_i^{\frac{1}{4}}>\frac{1}{3} , \quad i=1,3. \end{align}\]
Collecting the estimates above, we find \[\begin{align} &-\sum_{i\in\{1,3\}}\frac{\delta_i}{2\mathfrak m_i}|\dot{X}_i|^2 +\mathcal{B}^{\text{sh}}+\mathcal{B}_2-\mathfrak G-\frac{3}{4}D\\ &\quad\le\; -\alpha\sum_{i\in\{1,3\}}\mathcal{G}_i^S +C\delta_1^{\frac{4}{3}}\bigl(\delta_C^{\frac{4}{3}}+\delta_3^{\frac{4}{3}}\bigr)e^{-C\delta_1t}+ C\delta_3^{\frac{4}{3}}\bigl(\delta_C^{\frac{4}{3}}+\delta_1^{\frac{4}{3}}\bigr)e^{-C\delta_3t} \\ &\qquad +\left(\sum_{i\in\{1,3\}}C\delta_i^2e^{-C\delta_i t}+\frac{C}{\delta_*t^2}\right)\int_{\mathbb{R}}\eta(U|\bar U)\,dx -\frac{3}{4}\int_{\mathbb{R}}a\frac{\mu(\theta)}{v}\sum_{k=2}^3\psi_{kx}^2\,dx, \end{align}\] for some positive constant \(\alpha=O(1)\). This proves Lemma 12. ◻
In this subsection, we estimate the remaining macroscopic error terms \[\mathcal{B}_3,\dots,\mathcal{B}_6,\, \mathcal{B}^{\text{res}}, \mathcal{S}_1,\, \mathcal{S}_2.\] Here the term \(\mathcal{B}_2\) has already been incorporated into the dominant combination treated in the previous subsection. The terms considered below are all of lower order and will be controlled either by the dissipation \(\mathcal{D}_{\mathrm{mac}}(U)\), or by the smallness of the wave strengths and the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 .
We begin with the term involving the derivative of the weight function.
Lemma 14. For any sufficiently small constant \(\lambda>0\), there exists a constant \(C_\lambda>0\) such that \[\begin{align} \label{eq:B3-est} &|\mathcal{B}_3| \le \lambda \mathcal{D}_{\mathrm{mac}}(U) + C_\lambda \int_{\mathbb{R}}\bigl(\delta_1|\partial_x(v^{S_1})^{-X_1}|+\delta_3|\partial_x(v^{S_3})^{-X_3}|\bigr)|(\phi,\psi,\zeta)|^2\,dx \\ &\qquad + C_\lambda \int_{\mathbb{R}} \bigl(|\partial_x(v^{S_1})^{-X_1}|^2+|\partial_x(v^{S_3})^{-X_3}|^2+|u_{1x}^C|^2+|\theta_x^C|^2\bigr) |(\phi,\psi,\zeta)|^2\,dx. \end{align}\qquad{(20)}\]
Proof. By the definition of the weight \(a\), we have \[|a_x| \le \frac{C}{\sqrt{\delta_1}}|\partial_x(v^{S_1})^{-X_1}| + \frac{C}{\sqrt{\delta_3}}|\partial_x(v^{S_3})^{-X_3}|.\] Since \(\delta_1,\delta_3\) are sufficiently small and the shock derivatives are exponentially localized, the factor \(a_x\) is supported only in the shock region and is controlled by the shock profiles.
Using the smoothness of \(\alpha_{\rm{th}}\) and \(\mu\), together with \[\alpha_{\rm{th}}(\theta)-\alpha_{\rm{th}}(\bar\theta)=O(|\zeta|), \qquad \mu(\theta)-\mu(\bar\theta)=O(|\zeta|),\] and Young’s inequality, we obtain \[\begin{align} &|\mathcal{B}_3| \le \lambda \mathcal{D}_{\mathrm{mac}}(U) + C_\lambda \int_{\mathbb{R}}\bigl(\delta_1|\partial_x(v^{S_1})^{-X_1}|+\delta_3|\partial_x(v^{S_3})^{-X_3}|\bigr)|(\phi,\psi,\zeta)|^2\,dx \\ &\qquad + C_\lambda \int_{\mathbb{R}} \bigl(|\partial_x(v^{S_1})^{-X_1}|^2+|\partial_x(v^{S_3})^{-X_3}|^2+|u_{1x}^C|^2+|\theta_x^C|^2\bigr) |(\phi,\psi,\zeta)|^2\,dx. \end{align}\] This proves ?? . ◻
We next estimate the quadratic remainder terms.
Lemma 15. For any sufficiently small constant \(\lambda>0\), there exists a constant \(C_\lambda>0\) such that \[\begin{align} \label{eq:B4B5B6-est} &|\mathcal{B}_4|+|\mathcal{B}_5|+|\mathcal{B}_6|\nonumber\\ &\qquad \le \lambda \mathcal{D}_{\mathrm{mac}}(U) +C_\lambda \int_{\mathbb{R}} \bigl(|\partial_x(v^{S_1})^{-X_1}|^2+|\partial_x(v^{S_3})^{-X_3}|^2+|u_{1x}^C|^2+|\theta_x^C|^2\bigr) |(\phi,\psi,\zeta)|^2\,dx. \end{align}\qquad{(21)}\]
Proof. All the terms in \(\mathcal{B}_4\), \(\mathcal{B}_5\), and \(\mathcal{B}_6\) are at least quadratic in the perturbation variables. Moreover, each coefficient depends smoothly on the background state \(\bar U\), hence is uniformly bounded under the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 and the smallness of \(\delta_0\).
For example, \[\left| \frac{\mu(\bar\theta)}{v\bar v}\bar u_{1x}\psi_{1x}\phi \right| \le \lambda \frac{\mu(\bar\theta)}{v}\psi_{1x}^2 + C_\lambda |\bar u_{1x}|^2\,\phi^2,\] and similarly \[\left| \frac{\alpha_{\rm{th}}(\bar\theta)}{v\bar v\theta}\bar\theta_x\zeta_x\phi \right| \le \lambda \frac{\alpha_{\rm{th}}(\bar\theta)}{v\theta}\zeta_x^2 + C_\lambda |\bar\theta_x|^2\,\phi^2.\] All remaining terms are treated in the same way, using \[|\mu(\theta)-\mu(\bar\theta)|+|\alpha_{\rm{th}}(\theta)-\alpha_{\rm{th}}(\bar\theta)| \le C|\zeta|\] and the fact that \[|\bar u_{1x}|^2+|\bar\theta_x|^2 \le C\bigl(|\partial_x(v^{S_1})^{-X_1}|^2+|\partial_x(v^{S_3})^{-X_3}|^2+|u_{1x}^C|^2+|\theta_x^C|^2\bigr).\] Therefore ?? follows after summing all contributions. ◻
The contact-wave error term is estimated as follows.
Lemma 16. There exists a positive constant \(C\) such that \[\begin{align} \label{eq:B7-est} &|\mathcal{B}^{\mathrm{res}}| \nonumber\\ &\le \frac{C\delta_C}{1+t} \int_{\mathbb{R}}e^{-\frac{C_1|x|^2}{1+t}}|(\phi,\zeta)|^2\,dx + C(\delta_0+\varepsilon) \int_{\mathbb{R}} \bigl(|\partial_x(v^{S_1})^{-X_1}|+|\partial_x(v^{S_3})^{-X_3}|\bigr)|(\phi,\zeta)|^2\,dx. \end{align}\qquad{(22)}\]
Proof. This is immediate from the definition of \(\mathcal{B}^{\text{res}}\). ◻
We now estimate the profile-error terms \(\mathcal{S}_1\) and \(\mathcal{S}_2\).
Lemma 17. There exists a constant \(C>0\) such that \[\label{eq:S1S2-est} |\mathcal{S}_1|+|\mathcal{S}_2| \le C(\varepsilon+\delta_0)\left\{\frac{\delta_C}{\left(1+t\right)^{\frac{5}{4}}}+\delta_1\left(\delta_3+\delta_C\right)e^{-C\delta_1t}+\delta_3\left(\delta_1+\delta_C\right)e^{-C\delta_3t}\right\}\qquad{(23)}\]
Proof. Recall that \[\mathcal{S}_1=-\int_{\mathbb{R}}a\,\psi_1Q_1\,dx, \qquad \mathcal{S}_2=-\int_{\mathbb{R}}a\,\frac{\zeta}{\bar\theta}Q_2\,dx.\] Using the decomposition of \(Q_1\) and \(Q_2\) in 32 –33 , together with the Gaussian bound for the viscous contact wave and the exponential localization of the shock profiles, we obtain \[\begin{align} \left| \mathcal{S}_1\right|+\left| \mathcal{S}_2\right| &\leq \left(\bigl\lVert Q_1^I\bigr\rVert_{L^2}+\bigl\lVert Q_1^C\bigr\rVert_{L^2}+\bigl\lVert Q_2^I\bigr\rVert_{L^2}+\bigl\lVert Q_2^C\bigr\rVert_{L^2}\right)\bigl\lVert\left(\psi,\zeta\right)\bigr\rVert_{L^2}\\ &\leq C(\varepsilon+\delta_0)\left\{\frac{\delta_C}{\left(1+t\right)^{\frac{5}{4}}}+\delta_1\left(\delta_3+\delta_C\right)e^{-C\delta_1t}+\delta_3\left(\delta_1+\delta_C\right)e^{-C\delta_3t}\right\} \end{align}\] The desired estimate then follows from Young’s inequality. ◻
Collecting the previous lemmas, we obtain the following macroscopic estimate.
Proposition 3. For any sufficiently small constant \(\lambda>0\), there exist constants \(C>0\) and \(C_\lambda>0\) such that \[\label{eq:macro-error-final} \begin{align} &\sum_{i=3}^6 |\mathcal{B}_i| + |\mathcal{B}^{\mathrm{res}}| + |\mathcal{S}_1| + |\mathcal{S}_2|\\& \le \lambda \mathcal{D}_{\mathrm{mac}}(U) + C_\lambda \delta_C\frac{1}{1+t} \int_{\mathbb{R}}e^{-C_1|x|^2/(1+t)}|(\phi,\psi,\zeta)|^2\,dx\\ & + C_\lambda(\delta_0+\varepsilon) \int_{\mathbb{R}} \bigl(|\partial_x(v^{S_1})^{-X_1}|+|\partial_x(v^{S_3})^{-X_3}|\bigr) |(\phi,\psi,\zeta)|^2\,dx\\ & + C(\varepsilon+\delta_0)\left\{\frac{\delta_C}{\left(1+t\right)^{\frac{5}{4}}}+\delta_1\left(\delta_3+\delta_C\right)e^{-C\delta_1t}+\delta_3\left(\delta_1+\delta_C\right)e^{-C\delta_3t}\right\}. \end{align}\qquad{(24)}\]
We also need the contribution of the remaining modulation terms \[\sum_{i=1,3}\dot{X}_i\sum_{j=4}^6\mathcal{Y}_{ij},\] which are of lower order.
Lemma 18. There exists a constant \(C>0\) such that \[\label{eq:Y456-est} \left| \sum_{i=1,3}\dot{X}_i\sum_{j=4}^6 \mathcal{Y}_{ij} \right| \le \sum_{i=1,3}\frac{\delta_i}{8\mathfrak m_i}|\dot{X}_i|^2 + C(\delta_0+\varepsilon)^2\sum_{i=1,3}\mathcal{G}_i^S + C (\delta_0+\varepsilon)^2 \sum_{i=1,3}\delta_i^2e^{-C\delta_i t}.\qquad{(25)}\]
Proof. By the definitions of \(Y_{i4}\), \(Y_{i5}\), and \(Y_{i6}\), together with \[\Phi\!\left(\frac{v}{\bar v}\right)\sim \phi^2, \qquad \Phi\!\left(\frac{\theta}{\bar\theta}\right)\sim \zeta^2,\] and the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 , we obtain
\[\begin{align} \left| \mathcal{Y}_{i4}\right| \le & C \int \left| \partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\right| \left| \phi\right|^2 dx \\ \le & C \int \left| \varphi_i\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\right| \left| \phi\right|^2 dx + C \int \left| (1-\varphi_i^2)\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\right| \left| \phi\right|^2 dx \\ \le & C \mathcal{G}_i^S + C \int \left| (1-\varphi_i)\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\right|\left| \phi\right|^2 dx \\ \le & C \mathcal{G}_i^S + C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it}, \end{align}\]
\[\begin{align} \frac{C}{\delta_i}\left| \mathcal{Y}_{i4}\right|^2 \le& \frac{C\left| \mathcal{Y}_{i4}\right|}{\delta_i}\left| \int a\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}} \Phi\left(\frac{v}{\bar v}\right) dx\right|\\ \le& C\delta_i(\varepsilon+\delta_0)^2\left(\mathcal{G}_i^S +(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it}\right). \end{align}\]
By the similar argument for \(Y_{i5}\),
\[\label{eq:Y45-est} \frac{C}{\delta_i}\bigl(|\mathcal{Y}_{i4}|^2+|\mathcal{Y}_{i5}|^2\bigr) \le C\delta_i(\delta_0+\varepsilon)^2 \left(\mathcal{G}_i^S+(\delta_0+\varepsilon)^2\delta_i^2e^{-C\delta_i t}\right), \qquad i=1,3.\tag{93}\] Similarly, observe that \[\begin{align} \label{eq:Y6-est} \frac{C}{\delta_i}|\mathcal{Y}_{i6}|^2 \le & \frac{C}{\delta_i^2}\left(\int \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|\left| (\phi,\psi,\zeta)\right|^2 dx\right)^2 \nonumber\\ \le & C(\delta_0+\varepsilon)^2\left(\mathcal{G}_i^S+(\delta_0+\varepsilon)^2\delta_i^2e^{-C\delta_i t}\right), \qquad i=1,3. \end{align}\tag{94}\]
Therefore, by Young’s inequality, \[\begin{align} \left| \sum_{i=1,3}\dot{X}_i\sum_{j=4}^6\mathcal{Y}_{ij} \right| &\le \sum_{i=1,3}\left( \frac{\delta_i}{8\mathfrak m_i}|\dot{X}_i|^2 + \frac{C}{\delta_i}\sum_{j=4}^6|\mathcal{Y}_{ij}|^2 \right)\\ &\le \sum_{i=1,3}\frac{\delta_i}{8\mathfrak m_i}|\dot{X}_i|^2 + C(\delta_0+\varepsilon)^2\sum_{i=1,3}\mathcal{G}_i^S \\ &\qquad + C (\delta_0+\varepsilon)^2 \sum_{i=1,3}\delta_i^2e^{-C\delta_i t}, \end{align}\] which proves ?? . ◻
As a consequence, combining Proposition 3 with Lemma 18, we obtain \[\label{eq:macro-error-plus-shift} \begin{align} &\sum_{l=3}^6 |\mathcal{B}_l| + \mathcal{B}^{\text{res}} + |\mathcal{S}_1| + |\mathcal{S}_2| +\left| \sum_{i=1,3}\dot{X}_i\sum_{j=4}^6 \mathcal{Y}_{ij} \right|\\ &\le \sum_{i=1,3}\frac{\delta_i}{8\mathfrak M_i}|\dot{X}_i|^2 + \frac{1}{32} \mathcal{D}_{\mathrm{mac}}(U) + C \delta_C\frac{1}{1+t} \int_{\mathbb{R}}e^{-\frac{C_1|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx\\ &\quad + C(\delta_0+\varepsilon)\sum_{i=1,3}\mathcal{G}_i^S + C(\varepsilon+\delta_0)\left\{\frac{\delta_C}{\left(1+t\right)^{\frac{5}{4}}}+\delta_1\delta_0e^{-C\delta_1t}+\delta_3\delta_0e^{-C\delta_3t}\right\}. \end{align}\tag{95}\]
In this subsection, we estimate the kinetic error terms \[K_1,\dots,K_6\] appearing in the weighted entropy identity 86 . These terms arise from the microscopic part of the perturbation and will be controlled by the microscopic dissipation together with the smallness of the macroscopic perturbation and the exponential localization of the composite wave.
For convenience, we introduce the microscopic dissipation functional \[\label{eq:mic-diss} \mathcal{D}_{\mathrm{mic}}(t) := \int_{\mathbb{R}} a(t,x)\bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx.\tag{96}\]
We first estimate the terms involving the difference \[\begin{align} \label{eq:pi1w} \widetilde{\Pi}_1:=\,\Pi_1-(\Pi_1^{S_1})^{-X_1}-(\Pi_1^{S_3})^{-X_3}. \end{align}\tag{97}\]
Lemma 19. There exists a positive constant \(C\) such that \[\begin{align} \begin{aligned} &|K_1|+|K_2|+|K_3|+|K_4|+|K_5|\\ &\quad \le\; C(\delta_0+\varepsilon)\sum_{i\in\{1,3\}}\delta_i|\dot{X}_i|^2 + C\delta_0\sum_{i\in\{1,3\}}\mathcal{G}_i^S + \frac{1}{20}\mathcal{D}_{\mathrm{mac}}(U) + C(\delta_0+\varepsilon)\mathcal{D}_{\mathrm{mic}}(t) \\ &\qquad + C\delta_0(\delta_0+\varepsilon)\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr) + C\frac{\delta_C}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0x^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx\\ &\qquad + \frac{C\delta_C}{(1+t)^{\frac{5}{4}}} + C\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx . \end{aligned} \label{eq:K1245-est} \end{align}\qquad{(26)}\]
Proof. Control of \(K_4\). By definition, \[K_4 = -\iint a\psi_1\,\xi_1^2 \widetilde{\Pi}_{1x}\,d\xi\,dx.\] Integrating by parts in \(x\), we obtain \[\label{eq:K4-ibp} K_4 = \iint (a\psi_1)_x\,\xi_1^2 \widetilde{\Pi}_1\,d\xi\,dx.\tag{98}\] Hence, for arbitrary \(\alpha,\beta>0\), \[\begin{align} |K_4| \le\;& \frac{\alpha}{2}\int_{\mathbb{R}}(a_x\psi_1)^2\,dx +\frac{\alpha^{-1}}{2}\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2 \widetilde{\Pi}_1\,d\xi \right)^2dx \nonumber\\ &+ \frac{\beta}{2}\int_{\mathbb{R}}(a\psi_{1x})^2\,dx +\frac{\beta^{-1}}{2}\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2 \widetilde{\Pi}_1\,d\xi \right)^2dx. \label{eq:K4-Young} \end{align}\tag{99}\]
We now decompose the perturbative microscopic flux. Recall that \[\begin{align} \mathcal{N}(\widetilde{G},\widetilde{G}) =&-\mathcal{N}\bigl((G^{S_1})^{-X_1},\widetilde{G}\bigr)-\mathcal{N}\bigl(\widetilde{G},(G^{S_1})^{-X_1}\bigr)-\mathcal{N}\bigl((G^{S_1})^{-X_1},(G^{S_1})^{-X_1}\bigr)+\mathcal{N}(G,G)\nonumber\\ &-\mathcal{N}\bigl(\widetilde{G},(G^{S_3})^{-X_3}\bigr)-\mathcal{N}\bigl((G^{S_1})^{-X_1},(G^{S_3})^{-X_3}\bigr)-\mathcal{N}\bigl((G^{S_3})^{-X_3},\widetilde{G}\bigr)\nonumber\\ &-\mathcal{N}\bigl((G^{S_3})^{-X_3},(G^{S_3})^{-X_3}\bigr)-\mathcal{N}\bigl((G^{S_3})^{-X_3},(G^{S_1})^{-X_1}\bigr). \label{eq:Q-tilde-decomp} \end{align}\tag{100}\] Accordingly, \[\begin{align} & \widetilde{\Pi}_1 = L_M^{-1} \left( \widetilde{G}_t-\frac{u_1}{v}\widetilde{G}_x+\frac{1}{v}P_1(\xi_1\widetilde{G}_x)-\mathcal{N}(\widetilde{G},\widetilde{G}) \right) \nonumber\\ &\qquad -L_M^{-1} \left[ \mathcal{N}\bigl(\widetilde{G},(G^{S_1})^{-X_1}+(G^{S_3})^{-X_3}\bigr) + \mathcal{N}\bigl((G^{S_1})^{-X_1}+(G^{S_3})^{-X_3},\widetilde{G}\bigr) \right] \nonumber\\ &\qquad -L_M^{-1} \left[ \mathcal{N}\bigl((G^{S_1})^{-X_1},(G^{S_3})^{-X_3}\bigr) + \mathcal{N}\bigl((G^{S_3})^{-X_3},(G^{S_1})^{-X_1}\bigr) \right] \nonumber\\ &\qquad -\dot{X}_1(L_{1}^{S})^{-1}\partial_x(G^{S_1})^{-X_1} -\dot{X}_3(L_{3}^{S})^{-1}\partial_x(G^{S_3})^{-X_3} +J, \label{eq:Pi-perturb} \end{align}\tag{101}\] where \[\begin{align} J:=\;& \sum_{i\in\{1,3\}} \bigl(L_M^{-1}-(L_{i}^{S})^{-1}\bigr) \left((G^{S_i})_t^{-X_i}-\mathcal{N}\bigl((G^{S_i})^{-X_i},(G^{S_i})^{-X_i}\bigr)\right) \nonumber\\ &+ \sum_{i\in\{1,3\}} \left( \frac{(u_1^{S_i})^{-X_i}}{(v^{S_i})^{-X_i}}(L_{i}^{S})^{-1} -\frac{u_1}{v}L_M^{-1} \right)\partial_x(G^{S_i})^{-X_i} \nonumber\\ &+ \sum_{i\in\{1,3\}} \left( \frac{1}{v}L_M^{-1}P_1\xi_1 -\frac{1}{(v^{S_i})^{-X_i}}(L_{i}^{S})^{-1}P_1^{S_i}\xi_1 \right)\partial_x(G^{S_i})^{-X_i}. \label{eq:J-term} \end{align}\tag{102}\]
Using the weighted inverse estimate for \(L_M^{-1}\) and the collision estimates from Appendix A, we have \[\begin{align} \int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2L_M^{-1}\widetilde{G}_t\,d\xi \right)^2dx &\le C\iint\frac{(1+|\xi|)^{-1}|\widetilde{G}_t|^2}{M_\#}\,d\xi\,dx, \tag{103} \\ \int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2L_M^{-1}\left(\frac{u_1}{v}\widetilde{G}_x\right)\,d\xi \right)^2dx &\le C\iint\frac{(1+|\xi|)^{-1}|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx, \tag{104} \\ \int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2L_M^{-1}\left(\frac{1}{v}P_1(\xi_1\widetilde{G}_x)\right)\,d\xi \right)^2dx &\le C\iint\frac{(1+|\xi|)^{-1}|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx. \tag{105} \end{align}\] Moreover, \[\begin{align} & \int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2L_M^{-1}\mathcal{N}(\widetilde{G},\widetilde{G})\,d\xi \right)^2dx \nonumber \\ &\qquad \le C(\delta_0+\varepsilon)\mathcal{D}_{\text{mic}} + C\delta_C^4 \left( \frac{1}{(1+t)^4}+\frac{1}{(1+t)^2} \right) \int_{\mathbb{R}}e^{-c_0x^2/(1+t)}\,dx. \label{eq:K4-QGG} \end{align}\tag{106}\]
Here we used \[\begin{align} \label{eq:GCe} \bigl\lVert\widetilde{G}_C\bigr\rVert_{\nu,M_\#}^2 \approx |(u_{1x}^C,\theta_x^C)|^2. \end{align}\tag{107}\]
Similarly, \[\begin{align} &\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2L_M^{-1}\mathcal{N}\bigl(\widetilde{G},(G^{S_1})^{-X_1}\bigr)\,d\xi \right)^2dx \nonumber\\ &\qquad \le C\delta_1^2\mathcal{D}_{\text{mic}} + C\int |(u_{1x}^C,\theta_x^C)|^2 |\partial_x\bigl((v^{S_1})^{-X_1}\bigr)|^2\,dx, \label{eq:K4-mixed} \end{align}\tag{108}\] and the same estimate holds for the remaining mixed and interaction terms involving \((G^{S_3})^{-X_3}\).
Next, we estimate the term \(J\). Observe that \[L_M\bigl(L_M^{-1}-(L_{1}^{S})^{-1}\bigr)h = \mathcal{N}(M_1-M,(L_{1}^{S})^{-1}h)+\mathcal{N}((L_{1}^{S})^{-1}h,M_1-M)\] and \[\begin{align} &L_M (L_{1}^{S})^{-1} \bigl((G^{S_{1}})^{-X_{1}}\bigr)_x \\ &\quad = \mathcal{N}\Bigl(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}},(L_{1}^{S})^{-1} \partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\Bigr) + \mathcal{N}\Bigl(\bigl(M^{S_{1}}\bigr)^{-X_{1}},(L_{1}^{S})^{-1} \partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\Bigr)\\ &\qquad + \mathcal{N}\Bigl((L_{1}^{S})^{-1} \partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}\Bigr)+\mathcal{N}\Bigl((L_{1}^{S})^{-1} \partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(M^{S_{1}}\bigr)^{-X_{1}}\Bigr)\\ &\quad =\mathcal{N}\Bigl(M- \bigl(M^{S_{1}}\bigr)^{-X_{1}},(L_{1}^{S})^{-1} \partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\Bigr)\\ &\qquad +\mathcal{N}\Bigl((L_{1}^{S})^{-1} \partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},M-\bigl((M^{S_{1}})^{-X_{1}}\bigr)\Bigr) +\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}. \end{align}\] Using the identity \[M(a)-M(a') = \int_0^1 D_aM(a_s)\,(a-a')\,ds, \qquad a_s:=a'+s(a-a'),\] with \(a=(v,u,\theta)\) and \(a'=(v',u',\theta')\), we infer \[\bigl\lVert M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}\bigr\rVert_{\nu,M_\#}^2 \le C\Bigl|\bigl(v-\bigl(v^{S_{1}}\bigr)^{-X_{1}},u-\bigl(u^{S_{1}}\bigr)^{-X_{1}},\theta-\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\bigr)\Bigr|^2.\]
Therefore, \[\begin{align} &\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1^2\bigl(L_M^{-1}-(L_{1}^{S})^{-1}\bigr)\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\,d\xi \right)^2dx\nonumber\\ &\qquad \le C\delta_1 \int_{\mathbb{R}}\left|\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|^2 \left|\left(v-\bigl(v^{S_{1}}\bigr)^{-X_{1}},u-\bigl(u^{S_{1}}\bigr)^{-X_{1}},\theta-\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\right)\right|^2\,dx. \label{eq:J-est1} \end{align}\tag{109}\] Using the decomposition \[\begin{align} &\left(v-\bigl(v^{S_{1}}\bigr)^{-X_{1}},u-\bigl(u^{S_{1}}\bigr)^{-X_{1}} ,\theta-\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\right) \nonumber\\ &\qquad =\bigl(v-\overline{v},u-\overline{u},\theta-\overline{\theta}\bigr)+ \left(\bigl(v^{S_{3}}\bigr)^{-X_{3}}-v^*,\bigl(u^{S_{3}}\bigr)^{-X_{3}}-u^*,\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}-\theta^*\right)\nonumber\\ &\qquad \quad +\bigl(v^C-v_*,u^C-u_*,\theta^C-\theta_*\bigr) \end{align}\] the first part is controlled by \(\mathcal{G}_1^S\) of ?? , while the second part is estimated by Lemma 7. Hence, \[\begin{align} &\int_{\mathbb{R}}\left|\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|^2 \left|\left(v-\bigl(v^{S_{1}}\bigr)^{-X_{1}},u-\bigl(u^{S_{1}}\bigr)^{-X_{1}},\theta-\bigl(\theta^{S_{1}}\bigr)^{-X_{1}}\right)\right|^2\,dx\nonumber\\ &\qquad \le\; C\delta_1\mathcal{G}_1^S + C\delta_1^3e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx +C(\delta_1^2\delta_3^2+\delta_1^2\delta_C^2)\delta_1e^{-C\delta_1t}\nonumber \\ &\qquad \qquad +C\delta_1^3\delta_3(\delta_3e^{-C\delta_3t})\nonumber \\ &\qquad \le\;C\delta_1\mathcal{G}_1^S + C(\delta_0+\varepsilon)^2\delta_1^3e^{-C\delta_1 t}+C\delta_0^4\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3t}\bigr). \label{eq:interaction-est} \end{align}\tag{110}\]
The same estimate holds for the \(3\)-shock.
Collecting 99 –110 and choosing \(\alpha,\beta\) sufficiently small, we conclude that \[\begin{align} |K_4| \le\;& C\delta_0^4\sum_{i\in\{1,3\}}\delta_i|\dot{X}_i|^2 + C\delta_0\sum_{i\in\{1,3\}}\mathcal{G}_i^S + C\delta_0(\varepsilon+\delta_0)^2\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr) \nonumber\\ &+\frac{C\delta_C}{(1+t)^{\frac{5}{4}}} +\frac{C\delta_C^2}{1+t}\int_{\mathbb{R}}e^{-2c_0x^2/(1+t)}|(\phi,\zeta)|^2\,dx+\frac{1}{200}\mathcal{D}_{\mathrm{mac}}(U)\nonumber\\ &+C(\delta_0+\varepsilon)\mathcal{D}_{\mathrm{mic}}(t)+ C\int\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx. \label{eq:K4-final} \end{align}\tag{111}\]
Control of \(K_1\). By definition, \[K_1 = -\iint a\frac{\zeta}{\theta}\left(\xi_1\frac{|\xi|^2}{2}\right) \widetilde{\Pi}_{1x}\,d\xi\,dx.\] Integrating by parts in \(x\), we obtain \[K_1 = \iint \left(a\frac{\zeta}{\theta}\right)_x \left(\xi_1\frac{|\xi|^2}{2}\right) \widetilde{\Pi}_{1}\,d\xi\,dx.\] Hence, by Young’s inequality,
\[\begin{align} |K_1| \le\;& \underbrace{\frac{\alpha_1}{2}\int_{\mathbb{R}}\left(a_x\frac{\zeta}{\theta}\right)^2\,dx}_{K_{11}} +\frac{\alpha_1^{-1}}{2}\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1\frac{\left| \xi\right|^2}{2} \widetilde{\Pi}_{1}\,d\xi \right)^2dx \nonumber\\ &+ \underbrace{\frac{\alpha_2}{2}\int_{\mathbb{R}}\left(a\frac{\zeta_x}{\theta}\right)^2\,dx}_{K_{12}} +\frac{\alpha_2^{-1}}{2}\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1\frac{\left| \xi\right|^2}{2} \widetilde{\Pi}_{1}\,d\xi \right)^2dx \nonumber\\ &+ \underbrace{\frac{\alpha_3}{2}\int_{\mathbb{R}}\left(a\frac{\zeta\overline{\theta}_x}{\theta^2}\right)^2\,dx}_{K_{13}} +\frac{\alpha_3^{-1}}{2}\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1\frac{\left| \xi\right|^2}{2} \widetilde{\Pi}_{1}\,d\xi \right)^2dx \nonumber\\ &+ \underbrace{\frac{\alpha_4}{2}\int_{\mathbb{R}}\left(a\frac{\zeta\zeta_x}{\theta^2}\right)^2\,dx}_{K_{14}} +\frac{\alpha_4^{-1}}{2}\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3}\xi_1\frac{\left| \xi\right|^2}{2} \widetilde{\Pi}_{1}\,d\xi \right)^2dx. \label{eq:K1-Young} \end{align}\tag{112}\]
The terms \(K_{11}\) and \(K_{13}\) are controlled by \(\mathcal{G}_i^S\), and the terms \(K_{12}\) and \(K_{14}\) are controlled by the diffusion term \(\mathcal{D}_{\mathrm{mac}}(U)\).
By the same manner as \(K_4\),
\[\begin{align} & |K_1|\le\; C\delta_0^4\sum_{i\in\{1,3\}}\delta_i|\dot{X}_i|^2 + C\delta_0\sum_{i\in\{1,3\}}\mathcal{G}_i^S + C\delta_0(\varepsilon+\delta_0)^2\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr) \nonumber\\ & \qquad \quad+\frac{C\delta_C}{(1+t)^{\frac{5}{4}}} +\frac{C\delta_C^2}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0x^2}{1+t}}|(\phi,\zeta)|^2\,dx+\frac{1}{200}\mathcal{D}_{\mathrm{mac}}(U)\nonumber\\ & \qquad \quad +C(\delta_0+\varepsilon)\mathcal{D}_{\mathrm{mic}}(t)+ C\int\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx. \label{eq:K1-final} \end{align}\tag{113}\]
Control of \(K_2\). We write \[\begin{align} K_2 &= \iint a\frac{\zeta}{\theta} \bigg[ u_1\xi_1^2\Pi_{1x} -\sum_{i\in\{1,3\}}(u_1^{S_i})^{-X_i}\xi_1^2\partial_x(\Pi_1^{S_i})^{-X_i} \bigg]d\xi\,dx \nonumber\\ &= \iint a\frac{\zeta}{\theta}u_1\xi_1^2 \widetilde{\Pi}_{1x}\,d\xi\,dx \nonumber\\ &\quad + \sum_{i\in\{1,3\}} \iint a\frac{\zeta}{\theta}\bigl(u_1-(u_1^{S_i})^{-X_i}\bigr)\xi_1^2\partial_x\bigl((\Pi_1^{S_i})^{-X_i}\bigr)\,d\xi\,dx \nonumber\\ &=:J^{\text{mic}}_1+J^{\text{mic}}_2. \label{eq:K2-split} \end{align}\tag{114}\]
The term \(J_1^{\text{mic}}\) is treated exactly as \(K_4\). For \(J_2^{\text{mic}}\), using the exponential decay of \(\bigl((\Pi_1^{S_i})^{-X_i}\bigr)_x\) (See Lemma 4), we obtain \[\begin{align} |J_2^{\text{mic}}| \le\;& C\delta_1^2\mathcal{G}_1^S + C\delta_1^2(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}) \nonumber\\ &+ C\delta_3^2\mathcal{G}_3^S + C\delta_3^2(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}). \label{eq:J2-est} \end{align}\tag{115}\] Hence, \[\begin{align} |K_2| \le\;& C\delta_0^4\sum_{i\in\{1,3\}}\delta_i|\dot{X}_i|^2 + C\delta_0\sum_{i\in\{1,3\}}\mathcal{G}_i^S + \frac{1}{200}\mathcal{D}_{\mathrm{mac}}(U) + C(\delta_0+\varepsilon)\mathcal{D}_{\mathrm{mic}}(t) \nonumber\\ &+C\delta_0(\varepsilon+\delta_0)^2\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr)+\frac{C\delta_C}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0x^2}{1+t}}|(\phi,\zeta)|^2\,dx\nonumber\\ &+\frac{C\delta_C^4}{(1+t)^{\frac{5}{4}}}+ C\int\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx. \label{eq:K2-final} \end{align}\tag{116}\]
Finally, the mixed transverse kinetic terms \(K_3\) and \(K_5\) are controlled the same way as \(K_4\), since \[\int_{\mathbb{R}^3}\xi_1\xi_j\bigl((\Pi_1^{S_1})^{-X_1}+(\Pi_1^{S_3})^{-X_3}\bigr)\,d\xi=0, \qquad j=2,3.\] Therefore, \(K_3\) and \(K_5\) have the same bound as \(K_4\). Summing the above estimates yields ?? . ◻
Finally, we estimate the quadratic microscopic interaction term.
Lemma 20. There exists a positive constant \(C\) such that \[\label{eq:K6-est} |K_6| \le C\delta_0\sum_{i=1,3}\mathcal{G}_i^S + \frac{C\delta_C}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0x^2}{1+t}}|(\phi,\zeta)|^2\,dx.\qquad{(27)}\]
Proof. Using the exponential decay of \((\Pi_1^{S_i})^{-X_i}\) (See Lemma 4) and Young’s inequality, we obtain \[\begin{align} |K_6| &\le C \sum_{i\in\{1,3\}} \iint a\frac{\zeta^2}{\theta\bar\theta} \left| \xi_1\left(\frac{|\xi|^2}{2}-(u_1^{S_i})^{-X_i}\xi_1\right) \partial_x(\Pi_1^{S_i})^{-X_i} \right|\,d\xi\,dx\\ &\le C\sum_{i\in\{1,3\}} \int \left| \zeta\right|^2 \left\{\left| \int \xi_1\frac{\left| \xi\right|^2}{2}\partial_x\bigl(\Pi_1^{S_{i}}\bigr)^{-X_{i}} d\xi\right|+\left| \int \xi_1^2\partial_x\bigl(\Pi_1^{S_{i}}\bigr)^{-X_{i}} d\xi\right|\right\}dx\\ &\le C \sum_{i\in\{1,3\}} \delta_i^2 \int_{\mathbb{R}}|\partial_x(v^{S_i})^{-X_i}|\,\zeta^2\,dx. \end{align}\] The right-hand side is bounded by \[C\delta_0\sum_{i=1,3}\mathcal{G}_i^S + \frac{C\delta_C}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0x^2}{1+t}}|(\phi,\zeta)|^2\,dx + C\delta_0(\varepsilon+\delta_0)^2\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr),\] which proves ?? . ◻
Collecting the above estimates, we obtain the following proposition.
Proposition 4. There exists a positive constant \(C\) such that \[\begin{align} \begin{aligned} \sum_{j=1}^6 |K_j| \le&\; C\delta_0\sum_{i\in\{1,3\}}\delta_i|\dot{X}_i|^2+C\delta_0\sum_{i\in\{1,3\}}\mathcal{G}_i^S+\frac{1}{20}\mathcal{D}_{\mathrm{mac}}(U)+C(\delta_0+\varepsilon)\mathcal{D}_{\mathrm{mic}}(t)\\ & +C\delta_0(\delta_0+\varepsilon)\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr)+\frac{C\delta_C}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0x^2}{1+t}}|(\phi,\zeta)|^2\,dx\\ & +C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C\int\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx. \end{aligned} \label{eq:micro-error-final} \end{align}\qquad{(28)}\]
Proof. Lemma 19 already gives the stated bound for \(K_1\), \(K_2\),\(K_3\), \(K_4\), and \(K_5\). Lemma 20 provides the corresponding bounds for the remaining term \(K_6\). Adding these inequalities yields ?? . ◻
Combining Lemma 12, Proposition 3, Lemma 18, and Proposition 4, we arrive at the following preliminary zeroth-order inequality.
Lemma 21. There exist positive constants \(\alpha_0\) and \(C\) such that \[\begin{align} \begin{aligned} &\frac{d}{dt}\int_{\mathbb{R}}a\,\eta(U\mid\bar U)\,dx + \alpha_0\sum_{i=1,3}\mathcal{G}_i^S+\frac{1}{40}\mathcal{D}_{\mathrm{mac}}(U)+\sum_{i=1,3}\frac{\delta_i}{8\mathfrak m_i}|\dot{X}_i|^2\\ &\,\le \left( \sum_{i=1,3}C\delta_i^2e^{-C\delta_i t} +\frac{C}{\delta_*t^2} \right) \int_{\mathbb{R}}\eta(U\mid\bar U)\,dx + C\delta_0\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr)\\ &\quad +C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} +C\frac{\delta_C}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\zeta)|^2\,dx+C(\delta_0+\varepsilon)\mathcal{D}_{\mathrm{mic}}(t)\\ &\quad+ C\int\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx. \end{aligned} \label{eq:zero-prelim} \end{align}\qquad{(29)}\]
Proof. See Lemma 12, Lemma 18, Proposition 3 and Proposition 4. Combining ?? , ?? , and ?? and choosing \(\delta_0+\varepsilon\) sufficiently small, we absorb the lower-order shock terms into the principal coercive term \(\sum_i\mathcal{G}_i^S\), and the dissipation contributions into \(\mathcal{D}_{\mathrm{mac}}(U)\). This proves ?? . ◻
Lemma 22 (Short-time estimates). For \(t\le 1\), there exist constants \(C>0\) and \(\widetilde{c}_0>0\) such that \[\begin{align} \begin{aligned}\label{eq:final-short-estimate} &\left.\int \eta(U\mid\bar{U}) dx\right|_{t=1} +\widetilde{c}_0\int_0^1 \left[ \sum_{i=1,3}\mathcal{G}_i^S(s) + \mathcal{D}_{\mathrm{mac}}(U)(s) + \sum_{i=1,3}\delta_i|\dot{X}_i(s)|^2\right] ds \\ &\le \left.\int \eta(U\mid\bar{U}) dx\right|_{t=0} + C(\delta_0+\varepsilon) \int_0^1 \int \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#} \,dx\,ds \\ &\qquad +C\int_0^1 \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx\,ds + C\delta_0. \end{aligned} \end{align}\qquad{(30)}\]
Proof. Recall that 86 ,
\[\begin{align} \label{eq:energy2-1} \frac{d}{dt}\int a\eta(U\mid\bar{U}) dx \le \sum_{i\in\{1,3\}}\dot{X}_i\mathcal{Y}_i(U)+\sum_{l=1}^6 \mathcal{B}_l + \mathcal{S}_1+\mathcal{S}_2+ \sum_{l=1}^6 K_l -\mathfrak G(U)-\mathcal{D}_{\mathrm{mac}}(U). \end{align}\tag{117}\]
For any \(\lambda>0\), rearrange 117 ,
\[\begin{align} \label{eq:energy2-re} &\frac{d}{dt}\int a\eta(U\mid\bar{U}) dx + \sum_{i\in\{1,3\}}\frac{\delta_i}{4\mathfrak m_i}\left| \dot{X}_i\right|^2 +\frac{1}{2}\mathcal{D}_{\mathrm{mac}}(U) +\lambda \sum_{i\in\{1,3\}}\mathcal{G}_i^S \nonumber\\ &\le \sum_{i\in\{1,3\}} \frac{C}{\delta_i}\sum_{j=4}^6 |\mathcal{Y}_{ij}|^2 + \sum_{l=1}^6 \mathcal{B}_l + \mathcal{S}_1 + \mathcal{S}_2 + \sum_{l=1}^6 K_l -\mathfrak G(U) - \frac{1}{2}\mathcal{D}_{\mathrm{mac}}(U) +\lambda \sum_{i\in\{1,3\}}\mathcal{G}_i^S. \end{align}\tag{118}\]
For \(t\le 1\), we obtain the following rough estimate using 95 , ?? and the bootstrap assumptions.
\[\begin{align} \label{eq:coarsebd} \begin{aligned} &\sum_{i=1,3}\left(\frac{C}{\delta_i}\sum_{j=4}^6\left| \mathcal{Y}_{ij}\right|^2\right)+\sum_{l=1}^6 \left| \mathcal{B}_l\right| + \left| \mathcal{S}_1\right| + \left| \mathcal{S}_2\right| + \sum_{l=1}^6 \left| K_l\right| \\ &\qquad - \frac{1}{2}\mathcal{D}_{\mathrm{mac}}(U) - \mathfrak G(U) + \lambda \sum_{i\in\{1,3\}}\mathcal{G}_i^S\\ &\qquad \le C_\lambda \delta_0 + C(\delta_0+\varepsilon) \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx + C\int\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx. \end{aligned} \end{align}\tag{119}\] Using 119 , we have ?? . ◻
In this subsection, we estimate the microscopic energy associated with \(\widetilde{G}_{\text{rem}}\) and recover the microscopic dissipation needed to close the zeroth-order energy estimate.
Recall that \[\widetilde{G}=\widetilde{G}_{C}+\widetilde{G}_{\text{rem}}, \qquad \widetilde{G}_C = \frac{3}{2v\theta}L_M^{-1}P_1 \left[ \xi_1M\left(\xi_1u_{1x}^C+\frac{|\xi-u|^2}{2\theta}\theta_x^C\right) \right].\] We also recall that the weighted microscopic dissipation introduced in the previous subsection is \[\mathcal{D}_{\mathrm{mic}}(t) = \int_{\mathbb{R}} a(t,x)\bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx.\] Since \(a(t,x)\) is uniformly positive and bounded for sufficiently small \(\delta_0\), this quantity is equivalent to the unweighted microscopic norm \[\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx.\] For this reason, and in order to match Lemma 21, we work in this subsection with the unweighted microscopic energy \[\label{eq:Emic} \mathcal{E}_{\mathrm{mic}}(t) := \int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{M_\#}^2\,dx.\tag{120}\]
Subtracting the equation satisfied by \(\widetilde{G}_C\) from the microscopic perturbation equation, we obtain \[\begin{align} \left(\widetilde{G}_{\text{rem}}\right)_t-L_M\widetilde{G}_{\text{rem}} =\;& \sum_{i=1,3}\dot{X}_i \bigl((G^{S_{i}})^{-X_{i}}\bigr)_x +\frac{u_1}{v}\widetilde{G}_x -\frac{1}{v}P_1(\xi_1\widetilde{G}_x)\nonumber\\ &+\sum_{i=1,3}\left(\frac{u_1}{v}-\frac{(u_1^{S_i})^{-X_i}}{(v^{S_i})^{-X_i}}\right)\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\nonumber\\ &-\sum_{i=1,3} \left[ \frac{1}{v}P_1\bigl(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) - \frac{1}{(v^{S_i})^{-X_i}}P_1^{S_i}\bigl(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) \right] \nonumber\\ &+\mathcal{N}(\widetilde{G},\widetilde{G}) + 2\sum_{i=1,3}\mathcal{N}\bigl((G^{S_i})^{-X_i},\widetilde{G}\bigr) + 2\mathcal{N}\bigl((G^{S_1})^{-X_1},(G^{S_3})^{-X_3}\bigr)\nonumber\\ &+\sum_{i=1,3}\bigl(L_M-L_i^{S}\bigr)(G^{S_i})^{-X_i} \nonumber\\ &- \widetilde{G}_{Ct} -\frac{3}{2v\theta}P_1 \left[ \xi_1M\left(\xi\cdot\psi_x+\frac{|\xi-u|^2}{2\theta}\zeta_x\right) \right] +\mathcal{R}_{\mathrm{prof}}, \label{eq:G1-detailed} \end{align}\tag{121}\] where \[\begin{align} \mathcal{R}_{\mathrm{prof}} := \sum_{i=1,3} \left[ \frac{1}{(v^{S_i})^{-X_i}}P_1^{S_i}\bigl(\xi_1\partial_x\bigl((M^{S_i})^{-X_i}\bigr)\bigr) - \frac{3}{2v\theta}P_1 \left( \xi_1M\left(\partial_x\bigl((u_1^{S_i})^{-X_i}\bigr)+\frac{|\xi-u|^2}{2\theta}\partial_x\bigl((\theta^{S_i})^{-X_i}\bigr)\right) \right) \right]. \label{eq:Rprof} \end{align}\tag{122}\]
We now estimate the right-hand side term by term.
Proposition 5. There exists a positive constant \(C\) such that \[\begin{align} \begin{aligned} & \frac{d}{dt}\mathcal{E}_{\mathrm{mic}}(t) + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}\,dx \\ &\qquad \le\; C\delta_0\sum_{i=1,3}\mathcal{G}_i^S + C\delta_0(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C\|(\psi_x,\zeta_x)\|_{L^2_x}^2 \\ &\quad \qquad + C\delta_0\|(\phi_t,\psi_t,\zeta_t)\|_{L^2_x}^2 + C\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#} \,dx \\ &\quad \qquad + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C(\delta_0+\varepsilon)\delta_1^2e^{-C\delta_1 t} + C(\delta_0+\varepsilon)\delta_3^2e^{-C\delta_3 t}. \end{aligned} \label{eq:mic-diss-final} \end{align}\qquad{(31)}\]
Proof. Multiply 121 by \(\widetilde{G}_{\text{rem}}/M_\#\) and integrate over \(\mathbb{R}_x\times\mathbb{R}^3_\xi\). Since \(\widetilde{G}_{\text{rem}}\in\mathfrak Z_M^\perp\), the coercivity estimate for the linearized collision operator yields \[-\iint \frac{\widetilde{G}_{\text{rem}}L_M\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \ge \lambda_{\mathrm{mic}} \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx\] for some \(\lambda_{\mathrm{mic}}>0\).
We estimate the source terms one by one.
For the shift terms, Young’s inequality gives \[\begin{align} \iint \dot{X}_i (G^{S_i}_x)^{-X_i}\frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \le\;& \frac{\lambda_{\mathrm{mic}}}{32} \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx + C\delta_i^5|\dot{X}_i|^2 . \label{eq:mic-shift-est} \end{align}\tag{123}\] Similarly, \[\begin{align} \iint & \left(\frac{u_1}{v}-\frac{(u_1^{S_i})^{-X_i}}{(v^{S_i})^{-X_i}}\right) \bigl((G^{S_i})^{-X_i}\bigr)_x\frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \nonumber\\ & \, \le\;\frac{\lambda_{\mathrm{mic}}}{32}\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx +C\delta_i^2\int_{\mathbb{R}}|\partial_x\bigl((v^{S_i})^{-X_i}\bigr)|^2|(u_1-(u_1^{S_i})^{-X_i},\,v-(v^{S_i})^{-X_i})|^2\,dx . \label{eq:mic-mismatch-est} \end{align}\tag{124}\] Using the decomposition \[U-(U^{S_1})^{-X_1} = (U-\bar U)+(\bar U-(U^{S_1})^{-X_1}),\] the first part is controlled by \(\mathcal{G}_1^S\) of ?? , while the second part is estimated by Lemma 7. Thus the last integral is bounded by \[C\delta_0\mathcal{G}_i^S + C\delta_0^3\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr) + C\delta_i^3e^{-C\delta_i t}\int_{\mathbb{R}}\eta(U\mid \bar U)\,dx .\]
Next, note that \[P_1(\xi_1h)=\xi_1h-\sum_{j=0}^4\langle \xi_1h,\chi_j\rangle\chi_j.\] Hence \[\begin{align} -\iint \frac{1}{v}P_1(\xi_1\widetilde{G}_x)\frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \le\;& C\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + \frac{\lambda_{\mathrm{mic}}}{32} \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx . \label{eq:mic-P1Gx-est} \end{align}\tag{125}\] Also, \[\begin{align} & -\iint \frac{3}{2v\theta} P_1\left[ \xi_1M\left(\xi\cdot\psi_x+\frac{|\xi-u|^2}{2\theta}\zeta_x\right) \right] \frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \nonumber \\ & \qquad \le\; C\|(\psi_x,\zeta_x)\|_{L^2_x}^2 + \frac{\lambda_{\mathrm{mic}}}{64} \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx . \label{eq:mic-source-est} \end{align}\tag{126}\]
We next treat the profile-difference terms. A representative estimate is \[\begin{align} &\iint \left[ -\frac{3\bigl((u_1^{S_1})^{-X_1}\bigr)_x}{2v\theta}P_1(\xi_1^2M) + \frac{3\bigl((u_1^{S_1})^{-X_1}\bigr)_x}{2(v^{S_1})^{-X_1}(\theta^{S_1})^{-X_1}} P_1^{S_1}\xi_1^2(M^{S_1})^{-X_1} \right] \frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \nonumber\\ &\qquad\le C\delta_1^2\mathcal{G}_1^S + C\delta_0^3\bigl(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t}\bigr) + \frac{\lambda_{\mathrm{mic}}}{64} \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx . \label{eq:mic-profile-est} \end{align}\tag{127}\] The same estimate holds for the \(3\)-shock contribution. Likewise, the terms \[-\sum_{i=1,3}\left[ \frac{1}{v}P_1\bigl(\xi_1\bigl((G^{S_i})^{-X_i}\bigr)_x\bigr) - \frac{1}{(v^{S_i})^{-X_i}}P_1^{S_i}\bigl(\xi_1\bigl((G^{S_i})^{-X_i} \bigr)_x\bigr) \right]\] and \[\sum_{i=1,3}(L_M-L_1^S)(G^{S_i})^{-X_i}\] are profile-difference terms of the same type and are estimated in the same way.
For the nonlinear term, Lemmas 44, 45 in Appendix give \[\begin{align} \iint \mathcal{N}(\widetilde{G},\widetilde{G})\frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \le\;& C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx \nonumber\\ &+\frac{\lambda_{\mathrm{mic}}}{64}\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx +\frac{C\delta_C^4}{(1+t)^{\frac{5}{4}}} \label{eq:mic-Q-est} \end{align}\tag{128}\] Here we used \[\bigl\lVert\widetilde{G}_C\bigr\rVert_{\nu,M_\#}^2 \approx |(u_{1x}^C,\theta_x^C)|^2 .\] The mixed terms \(\mathcal{N}((G^{S_i})^{-X_i},\widetilde{G})\) and \(\mathcal{N}((G^{S_1})^{-X_1},(G^{S_3})^{-X_3})\) are controlled in the same way and contribute only lower-order shock terms and exponentially decaying remainders.
Finally, differentiating \(\widetilde{G}_C\) in time yields \[\iint \widetilde{G}_{Ct}\frac{\widetilde{G}_{\text{rem}}}{M_\#}\,d\xi\,dx \le C\delta_0\|(\phi_t,\psi_t,\zeta_t)\|_{L^2_x}^2 + \frac{\lambda_{\mathrm{mic}}}{64} \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx .\]
Collecting 123 –128 , choosing \(\delta_0+\varepsilon\) sufficiently small, and absorbing the microscopic coercive terms into the left-hand side, we obtain ?? . ◻
We now combine the preliminary zeroth-order inequality obtained in Lemma 21 with the microscopic energy estimate from Proposition 5. This yields the zeroth-order bound in the form needed for the full a priori estimate.
We begin with the equivalence between the relative entropy and the square of the perturbation variables.
Lemma 23. Under the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 , there exist positive constants \(c\) and \(C\) such that \[\label{eq:rel-entropy-equiv} c\,|(\phi,\psi,\zeta)|^2 \le \eta(U\mid\bar U) \le C\,|(\phi,\psi,\zeta)|^2.\qquad{(32)}\] Consequently, \[\label{eq:weighted-rel-entropy-equiv} c\int_{\mathbb{R}}a\,|(\phi,\psi,\zeta)|^2\,dx \le \int_{\mathbb{R}}a\,\eta(U\mid\bar U)\,dx \le C\int_{\mathbb{R}}a\,|(\phi,\psi,\zeta)|^2\,dx.\qquad{(33)}\]
Proof. Since \(v,\theta,\bar v,\bar\theta\) remain uniformly away from zero and infinity under 44 , the standard convexity property of \[\Phi(z)=z-1-\ln z\] implies \[\Phi\!\left(\frac{v}{\bar v}\right)\sim \left|\frac{\phi}{\bar v}\right|^2, \qquad \Phi\!\left(\frac{\theta}{\bar\theta}\right)\sim \left|\frac{\zeta}{\bar\theta}\right|^2.\] Together with the definition of \(\eta(U\mid\bar U)\), this yields ?? . Since the weight \(a\) is uniformly positive and bounded for sufficiently small \(\delta_0\), ?? follows. ◻
Lemma 24. For \(t\in[1,T]\), there exist constants \(c_0>0\) and \(C>0\) such that
\[\begin{align} \eta(U\mid\bar{U})(t)&+c_0\int_1^t\left[\sum_{i=1,3}\mathcal{G}_i^S(s)+\mathcal{D}_{\mathrm{mac}}(U)(s)+\sum_{i=1,3}\delta_i|\dot{X}_i(s)|^2\right]ds \nonumber\\ &\le C\eta(U\mid\bar{U})(1)+C\int_1^t \frac{\delta_C}{1+s}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+s}}|(\phi,\zeta)|^2\,dx\,ds\label{eq:zero-order-inter}\\ &\quad+C\delta_0\int_1^t \|(\phi_t,\psi_t,\zeta_t)\|_{L^2_x}^2\,ds +C(\delta_0+\varepsilon)\int_1^t \mathcal{D}_{\mathrm{mic}}\,ds \nonumber\\ &\quad+ C\int_1^t \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx\,ds + C\delta_0^{1/2}\nonumber \end{align}\qquad{(34)}\]
Proof. The right-hand side of ?? is integrable away from time 0, and hence contribute only \(O(\delta_0^{1/2})\) after time integration over \([1,t]\). ◻
Next, define the total zeroth-order energy \[\label{eq:E-zero} \mathcal{E}_0(t) := \int_{\mathbb{R}}a(t,x)\eta(U\mid\bar U)(t,x)\,dx + \kappa_1 \mathcal{E}_{\mathrm{mic}}(t),\tag{129}\] where \(\kappa_1>0\) is a sufficiently small constant to be chosen later.
By Lemma 23, the positivity and boundedness of \(a\), and the definition of \(\mathcal{E}_0(t)\), there exist positive constants \(c\) and \(C\) such that \[\begin{align} \label{eq:E0-equiv} &c\left( \|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 + \mathcal{E}_{\mathrm{mic}}(t) \right) \le \mathcal{E}_0(t)\nonumber\\ &\qquad \qquad \le C\left( \|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 + \mathcal{E}_{\mathrm{mic}}(t) \right). \end{align}\tag{130}\]
We now add Lemma 21 and \(\kappa_0\) times Proposition 5. Since \(a(t,x)\sim 1\) for sufficiently small \(\delta_0\), the weighted microscopic dissipation \(\mathcal{D}_{\mathrm{mic}}(t)\) is equivalent to the unweighted quantity \[\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx.\] Hence, choosing \(\kappa_1>0\) sufficiently small and then taking \(\delta_0+\varepsilon\) sufficiently small depending on \(\kappa_1\), we obtain the following proposition.
Proposition 6. Under the assumptions of Proposition 1, there exists a positive constant \(C\) such that for all \(t\in[0,T]\), \[\begin{align} \begin{aligned} &\|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 + \mathcal{E}_{\mathrm{mic}}(t) \\ &\quad +\int_0^t \left[ \sum_{i=1,3}\mathcal{G}_i^S(s) + \mathcal{D}_{\mathrm{mac}}(U)(s) + \sum_{i=1,3}\delta_i|\dot{X}_i(s)|^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx \right]ds \\ &\le C\left( \|(\phi,\psi,\zeta)(0)\|_{L^2_x}^2 + \mathcal{E}_{\mathrm{mic}}(0) +\delta_0^{1/2} \right) + C\delta_C\int_0^t \frac{1}{1+s}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+s}}|(\phi,\zeta)|^2\,dx\,ds \\ &\quad + C\int_0^t \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx\,ds + C\delta_0\int_0^t \|(\phi_t,\psi_t,\zeta_t)\|_{L^2_x}^2\,ds . \end{aligned} \label{eq:zero-order-prop} \end{align}\qquad{(35)}\]
Proof. See Lemma 22, Proposition 5, and Lemma 24. Integral ?? over \([0,T]\). Collecting all of these, we have the following estimate.
There exist constants \(c_0>0\) and \(C>0\) such that \[\begin{align} &\mathcal{E}_0(t)+ c_0\int_0^t \left[ \sum_{i=1,3}\mathcal{G}_i^S(s) + \mathcal{D}_{\mathrm{mac}}(U)(s) + \sum_{i=1,3}\delta_i|\dot{X}_i(s)|^2\right] ds\nonumber\\ &\qquad +c_0 \int_0^t \int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx ds\nonumber\\ &\le C\mathcal{E}_0(0)+ C\int_0^t \frac{\delta_C}{1+s}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+s}}|(\phi,\zeta)|^2\,dx\,ds+ C\delta_0\int_0^t \|(\phi_t,\psi_t,\zeta_t)\|_{L^2_x}^2\,ds\nonumber\\ &\qquad+C\int_0^t\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_t\bigr\rVert^2_{\nu,M_\#}+\bigl\lVert\widetilde{G}_x\bigr\rVert^2_{\nu,M_\#}\,dx\,ds +C\delta_0^{1/2}. \label{lacpiyof} \end{align}\tag{131}\]
The estimate ?? follows immediately from 120 , 130 and [eq:zero-order-final]. ◻
The high-order macroscopic estimates are derived by the standard differentiated energy method for the fluid part. Since the argument closely follows the established framework in [38], [37], and [62], we record only the main differentiated identities and the resulting estimates, emphasizing the terms that interact with the microscopic component and the dynamical shifts.
The proof of the energy estimate of \(\bigl\lVert(\phi_t,\psi_t,\zeta_t)\bigr\rVert_{L^2_x}^2\) follows from a standard energy estimate. For the reader’s conveinence, we provide the proof in the Appendix.
Lemma 25 (Time-derivative estimate). There exists \(C>0\) such that \[\begin{align} \begin{aligned}\label{eq:time-derivative-est} &\bigl\lVert\left(\phi_t,\psi_t,\zeta_t\right)\bigr\rVert_{L^2}^2 \\ &\leq C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i\left| \dot{X}_i\right|^2 + C\delta_0(\mathcal{G}_1^S+\mathcal{G}_3^S) + \frac{C\delta_C}{1+t} \int e^{-\frac{2c\left| x\right|^2}{1+t}}\left| \left(\phi,\psi,\zeta\right)\right|^2 dx \\ &\qquad + C\bigl\lVert\left(\phi_x,\psi_x,\zeta_x\right)\bigr\rVert_{L^2}^2 + \frac{C\delta_C}{(1+t)^{\frac{5}{4}}} + C\delta_0(\delta_0+\varepsilon)(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t})\\ &\qquad + C \int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \end{aligned} \end{align}\qquad{(36)}\]
The previous lemmas controls the full first-order spatial energy, but it does not provide a sufficiently direct coercive estimate for \(\phi_x\). To recover this missing control, we derive a compensating estimate by coupling the differentiated mass equation with the differentiated first momentum equation.
At this stage, it is important to avoid using the Chapman–Enskog expansion at the differentiated level, since such an expansion leads to a loss of regularity and obstructs the bootstrap closure. For this reason, all microscopic contributions will be estimated directly in terms of \(\widetilde{G}\), rather than through further Chapman–Enskog substitutions.
Lemma 26 (Compensating estimate for \(\phi_x\)). There exists \(C>0\) such that \[\begin{align} \label{eq:low-order-differential} &\frac{d}{dt}\int \left(\frac{2}{3}\mu(\overline{\theta})\phi_x^2-v\psi_1\phi_x\right) dx + \int \frac{2\theta}{3v}\phi_x^2 dx \nonumber\\ &\leq C(\delta_0+\varepsilon)\sum_{i=1,3} \mathcal{G}_i^S + C\delta_0(\delta_0+\varepsilon)(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t})+ C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} \nonumber \\ &\quad+ C(\delta_0+\varepsilon) \sum_{i=1,3}\delta_i\left| \dot{X}_i\right|^2 + C\bigl\lVert(\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 + C \bigl\lVert\phi_t\bigr\rVert_{L^2}^2 +C\varepsilon^2 \bigl\lVert\psi_{1xx}\bigr\rVert_{L^2}^2 \nonumber \\ & \quad+ C \frac{\delta_C}{1+t} \int e^{-\frac{2c\left| x\right|^2}{1+t}}\left| \left(\phi,\psi,\zeta\right)\right|^2\, dx +C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xt}\bigr\rVert_{\nu,M_\#}^2 \, dx \nonumber\\ &\quad+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \, dx. \end{align}\qquad{(37)}\]
Proof. We have \[\begin{align} &\left(\frac{2}{3}\mu(\overline{\theta})\phi_x^2-v\psi_1\phi_x\right)_t + v_t \psi_1 \phi_x + (v\psi_1\phi_t)_x-(v_x\psi_1+v\psi_{1x})\phi_t + \frac{2}{3}\frac{\theta}{v}\phi_x^2 \\ &+ \sum_{i=1,3}\dot{X}_i\phi_x\left\{-\frac{4}{3}\mu(\overline{\theta})\partial_{xx}\bigl(v^{S_{i}}\bigr)^{-X_{i}}+v\partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right\}\\ &=\frac{2}{3}v\phi_x\left(-\frac{\theta}{v^2}+\frac{\overline{\theta}}{\overline{v}^2}\right)\overline{v}_x+v\phi_xQ_1+v\phi_x \int \xi_1^2 \widetilde{\Pi}_{1x} \,d\xi \\ &+\frac{2}{3}\phi_x\zeta_x+\frac{2}{3}v\phi_x\overline{\theta}_x\left(\frac{1}{v}-\frac{1}{\overline{v}}\right)+\frac{2}{3}\mu'(\overline{\theta})\overline{\theta}_t\phi_x^2-\frac{4}{3}\mu(\overline{\theta})v\phi_x\overline{u}_{1xx}\left(\frac{1}{v}-\frac{1}{\overline{v}}\right)\\ &-\frac{4}{3}\phi_x\left(\mu(\theta)-\mu(\overline{\theta})\right)_xu_{1x}-\frac{4}{3}\phi_x\mu'(\overline{\theta})\overline{\theta}_x\left(\psi_{1x}-\frac{\phi}{\overline{v}}\overline{u}_{1x}\right)-\frac{4}{3}\mu(\overline{\theta})v\phi_x\overline{u}_{1x}\left(\frac{\overline{v}_x}{\overline{v}^2}-\frac{v_x}{v^2}\right)\\ &+\frac{4}{3}\phi_xv\left(\mu(\theta)-\mu(\overline{\theta})\right)\left(\frac{u_{1x}}{v}\right)_x+\frac{4}{3}\frac{\mu(\overline{\theta})}{v}\phi_x\psi_{1x}v_x. \end{align}\]
We single out the term involving \(\phi_t\), since it requires a direct use of the continuity equation. The remaining terms are estimated in the same way as the corresponding macroscopic error terms in the first-order spatial energy estimate.
\[\begin{align} -\int (v_x\psi_1+v\psi_{1x})\phi_t\,dx \le\;& \int \left| \phi_x\psi_1\phi_t\right| + \left| \bar v_x\psi_1\phi_t\right| + \left| \phi\psi_{1x}\phi_t\right| + \left| \bar v\psi_{1x}\phi_t\right|\,dx \\ \le\;& \Bigl(\frac{1}{128}+C(\varepsilon+\delta_0)\Bigr)\int \left| \phi_x\right|^2\,dx + C\|\phi_t\|_{L^2}^2 + C\|\psi_{1x}\|_{L^2}^2. \end{align}\] Here we use the continuity equation \[\phi_t=\psi_{1x}+\sum_{i=1,3}\dot{X}_i \partial_x(v^{S_i})^{-X_i},\] which yields \[\|\phi_t\|_{L^2}^2 \le C\|\psi_{1x}\|_{L^2}^2 + C\sum_{i=1,3}|\dot{X}_i|^2\|\partial_x(v^{S_i})^{-X_i}\|_{L^2}^2 \le C\|\psi_{1x}\|_{L^2}^2 + C\sum_{i=1,3}\delta_i^3|\dot{X}_i|^2.\] Therefore, \[\begin{align} -\int (v_x\psi_1+v\psi_{1x})\phi_t\,dx \le\;& \Bigl(\frac{1}{128}+C(\varepsilon+\delta_0)\Bigr)\int \left| \phi_x\right|^2\,dx + C\|\psi_{1x}\|_{L^2}^2 + C\sum_{i=1,3}\delta_i^3|\dot{X}_i|^2 . \end{align}\]
The remaining terms on the right-hand side are lower-order macroscopic error terms or microscopic coupling terms. They are estimated exactly as in the first-order spatial energy estimate, using the previously established bounds for \(Q_1\), the profile derivatives of \(\bar U\), and the microscopic moments involving \(\widetilde{\Pi}_1\). Collecting all these estimates, we obtain the desired inequality. ◻
We begin with the first-order spatial estimates for the macroscopic perturbation \((\phi,\psi,\zeta)\). The first lemma provides the basic differentiated \(H^1_x\)-energy inequality for \((\phi_x,\psi_x,\zeta_x)\), together with the corresponding dissipation on \(\psi_{xx}\) and \(\zeta_{xx}\). The remaining terms are lower-order error terms generated by the composite profile, the dynamical shifts, and the coupling with the microscopic component. For the reader’s conveinence, we provide the proof in the Appendix.
Lemma 27 (First-order spatial energy estimate). There exists \(C>0\) such that \[\begin{align} \begin{aligned}\label{eq:eoppz1} &\frac{d}{dt}\int \left(\frac{\overline{p}\theta}{2v}\phi_x^2+\frac{3\overline{p}v}{4}\psi_{1x}^2+\sum_{k=2}^3 \frac{\psi_{kx}^2}{2}+\frac{\zeta_x^2}{2}\right) dx \\ &\quad + \int 2\mu(\overline{\theta})\overline{p}\psi_{1xx}^2 + \sum_{k=2}^3 \frac{\mu(\theta)}{v} \psi_{kxx}^2 + \frac{\alpha_{\rm{th}}(\overline{\theta})}{v}\zeta_{xx}^2 dx \\ &\qquad \le C(\delta_0+\varepsilon) \sum_{i=1,3} \delta_i\left| \dot{X}_i\right|^2 + C \delta_0 (\mathcal{G}_1^S+\mathcal{G}_3^S) + C\frac{\delta_C}{1+t}\int e^{\frac{-2c\left| x\right|^2}{1+t}}\left| (\phi,\zeta)\right|^2 dx +C\delta_0\bigl\lVert\phi_{xx}\bigr\rVert_{L^2}^2\\ &\, \qquad + C(\delta_0+\varepsilon)\sum_{\left| \beta\right|=1}\bigl\lVert\partial^\beta(\phi,\psi,\zeta)\bigr\rVert_{L^2}^2 + C\frac{\delta_C}{(1+t)^{5/4}} +C(\varepsilon+\delta_0)\delta_0\left(\delta_3 e^{-C\delta_3t} + \delta_1 e^{-C\delta_1t}\right)\\ &\, \qquad + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu, M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu, M_\#}^2 dx +C\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \,dx. \end{aligned} \end{align}\qquad{(38)}\]
Lemma 28 (Second-order spatial estimate for \(\phi\)). There exists \(C>0\) such that \[\begin{align} \begin{aligned} &-\frac{d}{dt} \int \phi_{xx}\psi_{1x}\,dx + \int \frac{p}{2v} \phi_{xx}^2\,dx \\ &\leq C\delta_0 (\mathcal{G}^S_1+\mathcal{G}^S_3)+ C(\delta_0+\varepsilon)\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 + C \bigl\lVert(\psi_{1xx},\zeta_{xx})\bigr\rVert_{L^2}^2 \\ &\quad + C\delta_C \frac{1}{1+t} \int e^{-\frac{2c_0\left| x\right|^2}{1+t}}\left| \left(\phi,\zeta\right)\right|^2 dx +C(\delta_0+\varepsilon) \sum_{i=1,3}\delta_i\left| \dot{X}_i\right|^2\\ &\quad + C\delta_0(\delta_0+\varepsilon)(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t})+ C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} +C \int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2\, dx. \end{aligned} \label{eq:phi-xx-est} \end{align}\qquad{(39)}\]
Proof. Differentiating the first momentum equation in the perturbed system with respect to \(x\), we obtain \[\begin{align} \begin{aligned} &\psi_{1tx}+\left(p-\overline{p}\right)_{xx}+\left(\bar{p}-p^{S_{1},-X_{1}}-p^C-p^{S_{3},-X_{3}}\right)_{xx}-\sum_{i=1,3}\dot{X}_i \partial_{xx}\bigl(u_1^{S_{i}}\bigr)^{-X_{i}} \\ &= -Q_{1x}^C-\frac{4}{3}\left(\frac{\mu\left(\theta^C\right)u_{1x}^C}{v^C}\right)_{xx}-\int \xi_1^2 \widetilde{G}_{xx} \,d\xi . \end{aligned} \end{align}\] Multiplying this equation by \(-\phi_{xx}\) and integrating over \(x\in\mathbb{R}\), we start from \[-\int \phi_{xx}\psi_{1tx}\,dx.\] By integration by parts in time, \[\begin{align} -\int \phi_{xx}\psi_{1tx}\,dx &= -\frac{d}{dt}\int \phi_{xx}\psi_{1x}\,dx +\int \phi_{xxt}\psi_{1x}\,dx \\ &= -\frac{d}{dt}\int \phi_{xx}\psi_{1x}\,dx -\int \phi_{xt}\psi_{1xx}\,dx . \end{align}\] Hence, \[\begin{align} -\int \phi_{xx}\psi_{1tx}\,dx \le -\frac{d}{dt}\int \phi_{xx}\psi_{1x}\,dx +\frac{1}{128}\|\phi_{xt}\|_{L^2}^2 + C\|\psi_{1xx}\|_{L^2}^2. \end{align}\] Now differentiate the continuity equation \[\phi_t-\psi_{1x}-\sum_{i=1,3}\dot{X}_i \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}=0\] with respect to \(x\). Then \[\phi_{xt} = \psi_{1xx} + \sum_{i=1,3}\dot{X}_i \partial_{xx}\bigl(v^{S_{i}}\bigr)^{-X_{i}},\] so that \[\begin{align} \|\phi_{xt}\|_{L^2}^2 &\le C\|\psi_{1xx}\|_{L^2}^2 + C\sum_{i=1,3} |\dot{X}_i|^2 \|\partial_{xx}\bigl(v^{S_{i}}\bigr)^{-X_{i}}\|_{L^2}^2 \\ &\le C\|\psi_{1xx}\|_{L^2}^2 + C\sum_{i=1,3}\delta_i^5 |\dot{X}_i|^2 \\ &\le C\|\psi_{1xx}\|_{L^2}^2 + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i |\dot{X}_i|^2 . \end{align}\] Therefore, \[\begin{align} \label{eq:phixt-control} -\int \phi_{xx}\psi_{1tx}\,dx \le -\frac{d}{dt}\int \phi_{xx}\psi_{1x}\,dx + C\|\psi_{1xx}\|_{L^2}^2 + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i |\dot{X}_i|^2 . \end{align}\tag{132}\]
Next, note that \[\begin{align} \begin{aligned} \left(p-\overline{p}\right)_{xx} = -\frac{p}{v}\phi_{xx} +\frac{2}{3v}\zeta_{xx} -\frac{1}{v}\left(p-\overline{p}\right)\overline{v}_{xx} -\frac{\phi}{v}\overline{p}_{xx} -\frac{2v_x}{v}\left(p-\overline{p}\right)_x -\frac{2\overline{p}_x}{v}\phi_x . \end{aligned} \end{align}\] The leading term gives the desired coercivity: \[-\int \phi_{xx}\left(-\frac{p}{v}\phi_{xx}\right)\,dx = \int \frac{p}{v}\phi_{xx}^2\,dx .\] The remaining terms are lower-order error terms. For example, \[\begin{align} -\int \frac{2}{3v}\phi_{xx}\zeta_{xx}\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C\|\zeta_{xx}\|_{L^2}^2, \\ \int \frac{1}{v}\left(p-\overline{p}\right)\overline{v}_{xx}\phi_{xx}\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C\int \left| \overline{v}_{xx}\right|^2\left| (\phi,\zeta)\right|^2\,dx, \\ \int \frac{\phi\phi_{xx}}{v}\overline{p}_{xx}\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C\int \left| \overline{p}_{xx}\right|^2\left| \phi\right|^2\,dx, \\ \int \frac{2v_x\phi_{xx}}{v}\left(p-\overline{p}\right)_x\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C(\delta_0+\varepsilon)^2\|(\phi_x,\zeta_x)\|_{L^2}^2 \\ &\qquad + C(\delta_0+\varepsilon)^2\int \left| (\overline{\theta}_x,\overline{v}_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx, \\ \int \frac{2\overline{p}_x}{v}\phi_{xx}\phi_x\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C(\delta_0+\varepsilon)^2\|\phi_x\|_{L^2}^2 . \end{align}\]
We next estimate the profile-error and microscopic terms: \[\begin{align} -\int \phi_{xx} \left(\overline{p}-p^{S_{1},-X_{1}}-p^C-p^{S_{3},-X_{3}}\right)_{xx}\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C \|Q_{1x}\|_{L^2}^2, \\ \sum_{i=1,3} \int \dot{X}_i \partial_{xx}\bigl(u_1^{S_{i}}\bigr)^{-X_{i}} \phi_{xx}\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C\sum_{i=1,3} \delta_i^3 |\dot{X}_i|^2, \\ \int \phi_{xx} \left(Q_{1x}^C + \frac{4}{3}\left(\frac{\mu\left(\theta^C\right)u^C_{1x}}{v^C}\right)_{xx}\right)\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx + C \|Q_{1x}^C\|_{L^2}^2, \\ \int \phi_{xx} \int \xi_1^2 \widetilde{G}_{xx}\,d\xi\,dx &\le \frac{1}{128}\int \frac{p}{v}\phi_{xx}^2\,dx \\ &\qquad + C \int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 dx . \end{align}\]
Combining these bounds with 132 , we obtain \[\begin{align} \begin{aligned} & -\frac{d}{dt}\int \phi_{xx}\psi_{1x}\,dx +\int \frac{p}{2v}\phi_{xx}^2\,dx \\ &\quad \le C \|(\psi_{1xx},\zeta_{xx})\|_{L^2}^2 + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i |\dot{X}_i|^2 + C \int \left| (\overline{v}_{xx},\overline{p}_{xx})\right|^2\left| (\phi,\zeta)\right|^2\,dx + C \|Q_{1x}\|_{L^2}^2 \\ &\qquad + C \|Q_{1x}^C\|_{L^2}^2 + C(\delta_0+\varepsilon)^2 \|(\phi_x,\zeta_x)\|_{L^2}^2 + C(\delta_0+\varepsilon)^2 \int \left| (\overline{\theta}_x,\overline{v}_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx\\ &\qquad + C \int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 dx . \end{aligned} \end{align}\]
Finally, the terms involving \(Q_{1x}\), \(Q_{1x}^C\), \((\overline{v}_{xx},\overline{p}_{xx})\), and \((\overline{\theta}_x,\overline{v}_x)\) are estimated exactly as in the previous macroscopic energy bounds, using the profile decay estimates for the composite wave. In particular, \[\int \left| (\overline{v}_{xx},\overline{p}_{xx})\right|^2\left| (\phi,\zeta)\right|^2\,dx + \int \left| (\overline{\theta}_x,\overline{v}_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx\] is bounded by \[C\delta_0 (\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_C^2 \frac{1}{1+t}\int e^{-\frac{2c_0|x|^2}{1+t}}\left| (\phi,\zeta)\right|^2\,dx + C\delta_0^3(\delta_1e^{-C\delta_1 t}+\delta_Ce^{-Ct}+\delta_3e^{-C\delta_3 t}),\] while \[\|Q_{1x}\|_{L^2}^2+\|Q_{1x}^C\|_{L^2}^2\] is bounded by \[C\delta_0^3(\delta_1e^{-C\delta_1 t}+\delta_3e^{-C\delta_3 t})+C\frac{\delta_C^4}{(1+t)^{5/4}} + C(\varepsilon+\delta_0)\delta_3^2 e^{-C\delta_3t} + C(\varepsilon+\delta_0)\delta_1^2 e^{-C\delta_1t}.\] This proves ?? . ◻
Lemma 29 (Mixed derivative estimate). There exists \(C>0\) such that \[\begin{align} \begin{aligned} &\bigl\lVert\left(\phi_{xt},\psi_{xt},\zeta_{xt}\right)\bigr\rVert_{L^2}^2 \\ &\leq C \bigl\lVert\left(\phi_{xx},\psi_{xx},\zeta_{xx}\right)\bigr\rVert_{L^2}^2 + C(\delta_0+\varepsilon) \sum_{i=1,3}\delta_i\left| \dot{X}_i\right|^2 + C \delta_0 (\mathcal{G}^{S}_1+\mathcal{G}^S_3)\\ &\quad + C\delta_C \frac{1}{1+t} \int e^{-\frac{2c_0\left| x\right|^2}{1+t}}\left| \left(\phi,\psi,\zeta\right)\right|^2 dx+ C(\delta_0+\varepsilon)\bigl\lVert\left(\phi_x,\psi_x,\zeta_x\right)\bigr\rVert_{L^2}^2 \\ &\quad +C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \, dx\\ &\quad + C\delta_0(\delta_0+\varepsilon)(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t})+ C\frac{\delta_C}{(1+t)^{\frac{5}{4}}}. \end{aligned} \label{eq:mixed-derivative-est} \end{align}\qquad{(40)}\]
Proof. Differentiating the perturbed system with respect to \(x\), we obtain \[\begin{align} \begin{aligned} &\phi_{xt}-\psi_{1xx}-\sum_{i=1,3} \dot{X}_i \partial_{xx}\bigl(v^{S_{i}}\bigr)^{-X_{i}} = 0,\\ &\psi_{1tx} + \left(p-p^{S_1,-X_1}-p^C-p^{S_3,-X_3}\right)_{xx}-\sum_{i=1,3} \dot{X}_i \partial_{xx}\bigl(u_1^{S_{i}}\bigr)^{-X_{i}} \\ &\qquad \quad= -Q_{1x}^C-\frac{4}{3}\left(\frac{\mu\left(\theta^C\right)u_{1x}^C}{v^C}\right)_{xx}-\int \xi_1^2 \widetilde{G}_{xx} d\xi,\\ &\psi_{itx}=-\int \xi_1\xi_i \widetilde{G}_{xx} d\xi,\quad (i=2,3),\\ &\zeta_{tx} +\left(pu_{1x}-p^{S_1,-X_1}\partial_x\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}-p^Cu_{1x}^C-p^{S_3,-X_3}\partial_x\bigl(u_1^{S_{3}}\bigr)^{-X_{3}}\right)_x-\sum_{i=1,3}\dot{X}_i\partial_{xx}\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\\ &\qquad = -\frac{1}{2}\int \xi_1 \left| \xi\right|^2 \widetilde{G}_{xx} d\xi +u_{1x}\int \xi_1^2 \widetilde{G}_x d\xi +u_1\int \xi_1^2 \widetilde{G}_{xx} d\xi \\ &\qquad\quad +\sum_{i=1,3} \left(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right)_x\int \xi_1^2 \partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}} d\xi\\ &\qquad\quad +\sum_{i=1,3} \left(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right)\int \xi_1^2 \partial_{xx}\bigl(G^{S_{i}}\bigr)^{-X_{i}} d\xi\\ &\qquad\quad +\sum_{k=2}^3 u_{kx} \int \xi_1\xi_k \widetilde{G}_x d\xi+\sum_{k=2}^3 u_k \int \xi_1\xi_k \widetilde{G}_{xx} d\xi \\ &\qquad\quad-\left(\frac{\alpha_{\rm{th}}\left(\theta^C\right)\theta_x^C}{v^C}\right)_{xx}-\left\{\frac{4}{3}\mu\left(\theta^C\right)\frac{\left(u_{1x}^C\right)^2}{v^C}+Q_2^C\right\}_x . \end{aligned} \end{align}\]
We estimate \(\phi_{xt}\), \(\psi_{xt}\), and \(\zeta_{xt}\) separately.
Step 1: estimate of \(\phi_{xt}\). Multiplying the first equation by \(\phi_{xt}\) and integrating over \(x\), we get \[\begin{align} \|\phi_{xt}\|_{L^2}^2 &\le \frac{1}{128}\|\phi_{xt}\|_{L^2}^2 + C\|\psi_{1xx}\|_{L^2}^2 + \frac{1}{128}\|\phi_{xt}\|_{L^2}^2 + C\sum_{i=1,3}\delta_i^5|\dot{X}_i|^2. \end{align}\] Hence, \[\begin{align} \label{eq:phixt-est} \|\phi_{xt}\|_{L^2}^2 \le C\|\psi_{1xx}\|_{L^2}^2 + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2. \end{align}\tag{133}\]
Step 2: estimate of \(\psi_{1tx}\). Multiplying the differentiated first momentum equation by \(\psi_{1tx}\) and integrating over \(x\), we obtain \[\begin{align} \|\psi_{1tx}\|_{L^2}^2 \le\;& \frac{1}{128}\|\psi_{1tx}\|_{L^2}^2 + C\|(p-\bar p)_{xx}\|_{L^2}^2 + C\|Q_{1x}\|_{L^2}^2 + C\sum_{i=1,3}\delta_i^3|\dot{X}_i|^2 \\ &+ C\|Q_{1x}^C\|_{L^2}^2 + C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2\,dx . \end{align}\] Since \[(p-\bar p)_{xx} = -\frac{p}{v}\phi_{xx} +\frac{2}{3v}\zeta_{xx} -\frac{1}{v}(p-\bar p)\bar v_{xx} -\frac{\phi}{v}\bar p_{xx} -\frac{2v_x}{v}(p-\bar p)_x -\frac{2\bar p_x}{v}\phi_x,\] we have \[\begin{align} \|(p-\bar p)_{xx}\|_{L^2}^2 \le\;& C\|(\phi_{xx},\zeta_{xx})\|_{L^2}^2 + C(\delta_0+\varepsilon)^2\|(\phi_x,\zeta_x)\|_{L^2}^2 \\ &+ C\int \left| (\bar v_{xx},\bar p_{xx})\right|^2\left| (\phi,\zeta)\right|^2\,dx + C(\delta_0+\varepsilon)^2\int \left| (\bar v_x,\bar\theta_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx . \end{align}\] Therefore, \[\begin{align} \label{eq:psi1tx-est} \begin{aligned} \|\psi_{1tx}\|_{L^2}^2 \le\;& C\|(\phi_{xx},\zeta_{xx})\|_{L^2}^2 + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C(\delta_0+\varepsilon)^2\|(\phi_x,\zeta_x)\|_{L^2}^2 \\ &+ C\int \left| (\bar v_{xx},\bar p_{xx})\right|^2\left| (\phi,\zeta)\right|^2\,dx + C(\delta_0+\varepsilon)^2\int \left| (\bar v_x,\bar\theta_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx \\ &+ C\|Q_{1x}\|_{L^2}^2 + C\|Q_{1x}^C\|_{L^2}^2 + C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2\, dx . \end{aligned} \end{align}\tag{134}\]
Step 3: estimate of \(\psi_{itx}\), \(i=2,3\). Multiplying \[\psi_{itx}=-\int \xi_1\xi_i \widetilde{G}_{xx}\,d\xi\] by \(\psi_{itx}\) and integrating in \(x\), we get \[\label{eq:psiitx-est} \|\psi_{itx}\|_{L^2}^2 \le C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \, dx, \qquad i=2,3.\tag{135}\]
Step 4: estimate of \(\zeta_{tx}\). Multiplying the differentiated energy equation by \(\zeta_{tx}\) and integrating over \(x\), we obtain \[\begin{align} & \|\zeta_{tx}\|_{L^2}^2 \\ & \, \le C\Bigl\|\left(pu_{1x}-p^{S_1,-X_1}\partial_x\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}-p^Cu_{1x}^C-p^{S_3,-X_3}\partial_x\bigl(u_1^{S_{3}}\bigr)^{-X_{3}}\right)_x\Bigr\|_{L^2}^2 \\ &\quad + C\sum_{i=1,3}\delta_i^3|\dot{X}_i|^2 + C\|Q_{2x}\|_{L^2}^2 + C\|Q_{2x}^C\|_{L^2}^2 + C\|\theta_{xxx}^C\|_{L^2}^2 \\ &\quad + C\sum_{i=1,3}\int \left| \bigl(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\bigr)_x\right|^2 \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|^2\,dx\\ &\quad + C(\delta_0+\varepsilon)\sum_{i=1,3}\int \left| u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right|^2 \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|^2\,dx \\ &\quad + C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2\, dx + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\, dx. \end{align}\] Now \[\begin{align} &\left| \left(pu_{1x}-\bar p\,\bar u_{1x}\right)_x\right|\\ &\quad \le C \left| \psi_{1xx}\right| + C \left| (p-\bar p)_x\right|\left| (\bar u_{1x},\psi_{1x})\right| + C \left| \bar p_x\right|\left| \psi_{1x}\right| + C\left| (\phi,\zeta)\right|\left| \bar u_{1xx}\right|, \end{align}\] and therefore \[\begin{align} &\Bigl\|\left(pu_{1x}-\bar p\,\bar u_{1x}\right)_x\Bigr\|_{L^2}^2\\ &\quad \le C\|\psi_{1xx}\|_{L^2}^2 + C(\delta_0+\varepsilon)^2\|(\zeta_x,\psi_x,\phi_x)\|_{L^2}^2 \\ &\qquad + C(\delta_0+\varepsilon)^2\int \left| (\bar\theta_x,\bar v_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx + C\int \left| \bar u_{1xx}\right|^2\left| (\phi,\zeta)\right|^2\,dx . \end{align}\] Hence \[\begin{align} \label{eq:zetatx-est} \begin{aligned} & \|\zeta_{tx}\|_{L^2}^2 \\ & \quad \le C\|\psi_{1xx}\|_{L^2}^2 + C(\delta_0+\varepsilon)^2\|(\zeta_x,\psi_x,\phi_x)\|_{L^2}^2 + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 \\ &\qquad + C\int \left| (\bar\theta_x,\bar v_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx + C\int \left| \bar u_{1xx}\right|^2\left| (\phi,\zeta)\right|^2\,dx \\ &\qquad + C\|Q_{2x}\|_{L^2}^2 + C\|Q_{2x}^C\|_{L^2}^2 + C\|\theta_{xxx}^C\|_{L^2}^2 \\ &\qquad + C\sum_{i=1,3}\int \left| \partial_x\bigl(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\bigr)\right|^2 \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|^2\,dx \\ &\qquad + C(\delta_0+\varepsilon)\sum_{i=1,3}\int \left| u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right|^2 \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|^2\,dx \\ &\qquad + C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \, dx + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \, dx. \end{aligned} \end{align}\tag{136}\]
The profile terms in 134 and 136 are estimated exactly as in the previous macroscopic estimates. In particular, \[\int \left| (\bar v_{xx},\bar p_{xx},\bar u_{1xx})\right|^2\left| (\phi,\zeta)\right|^2\,dx + \int \left| (\bar\theta_x,\bar v_x)\right|^2\left| (\phi,\zeta)\right|^2\,dx\] is bounded by \[C\delta_0 (\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_C^2 \frac{1}{1+t}\int e^{-\frac{2c_0|x|^2}{1+t}}\left| (\phi,\psi,\zeta)\right|^2\,dx + C\delta_0^3(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}),\] while \[\|Q_{1x}\|_{L^2}^2+\|Q_{1x}^C\|_{L^2}^2+\|Q_{2x}\|_{L^2}^2+\|Q_{2x}^C\|_{L^2}^2+\|\theta_{xxx}^C\|_{L^2}^2\] is bounded by \[C\delta_0^3(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}) + C\frac{\delta_C^4}{(1+t)^{\frac{5}{4}}} + C(\varepsilon+\delta_0)\delta_3^2 e^{-C\delta_3t} + C(\varepsilon+\delta_0)\delta_1^2 e^{-C\delta_1t}.\] Finally, the shock-interaction terms are controlled by the already established wave-interaction bounds, giving \[\begin{align} & \sum_{i=1,3}\int \left| \bigl(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\bigr)_x\right|^2 \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|^2\,dx + (\delta_0+\varepsilon)\int \left| u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right|^2 \left| \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\right|^2\,dx\\ & \le C\delta_0(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^3(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}). \end{align}\]
We now turn to the high-order estimates for the microscopic component. In contrast to the macroscopic part, the main difficulty here is that spatial and temporal derivatives of the microscopic equation generate nontrivial commutator terms involving the linearized collision operator, the composite background profile, and the shock modulation. To close the high-order energy estimates, it is therefore necessary to isolate the basic microscopic identities first and then estimate the differentiated quantities \(\widetilde{G}_x\), \(\widetilde{G}_t\), and the second-order derivatives in a systematic way.
In this subsection, we collect the auxiliary microscopic estimates that will be used repeatedly in the proofs of the high-order bounds for \(\widetilde{G}_x\), \(\widetilde{G}_t\), and the second-order microscopic derivatives. The main purpose of these lemmas is to control the interaction between the differentiated microscopic terms and the composite background profile, especially near the shock layers where the microscopic part of the Boltzmann shock remains essential.
The first group of lemmas provides weighted interaction estimates between the perturbation of the macroscopic variables and generic microscopic quantities. These bounds allow us to convert factors such as \(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\), \(v_x-\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\), and their derivatives into the shock dissipation \(\mathcal{G}_i^S\), lower-order macroscopic norms, and exponentially decaying interaction remainders.
Lemma 30. For \(k\geq 0\) and \(\delta_1>0\), assume that \[\bigl\lVert H\bigr\rVert_{M_\#} \le C\,\delta_1^{\,k}\,\bigl|\bigl((v^{S_1})^{-X_1}\bigr)_x\bigr|.\] Then \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|v-\bigl(v^{S_1}\bigr)^{-X_1}\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& C\delta_1^{2k+2}\mathcal{G}_1^S + C\delta_1^{2k+4}e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx \\ &+ C\delta_1^{2k+3}\bigl(\delta_3^2e^{-C\delta_3 t}+\delta_0^2e^{-C\delta_1t}\bigr) + \frac{1}{\widetilde{\alpha}} \int \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx, \end{align}\] where \(\widetilde{\alpha}=O(1)\) and \(\mathcal{G}_1^S\) has been defined in ??
Proof. For convenience, we omit the shift \(X_1\). By Young’s inequality, for any \(\widetilde{\alpha}>0\), \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|v-v^{S_1}\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& \widetilde{\alpha} \int_{\mathbb{R}} |v-v^{S_1}|^2\bigl\lVert H\bigr\rVert_{M_\#}^2\,dx \\ &+ \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx . \end{align}\] Using the assumption on \(H\), we obtain \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|v-v^{S_1}\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& C\widetilde{\alpha}\,\delta_1^{2k} \int_{\mathbb{R}} |v-v^{S_1}|^2\,|(v^{S_1})_x|^2\,dx \\ &+ \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx . \end{align}\]
We now decompose \[v-v^{S_1} = \phi +(v^C-v_*)+(v^{S_3}-v^*),\] and therefore \[\begin{align} \int_{\mathbb{R}}|v-v^{S_1}|^2 |(v^{S_1})_x|^2\,dx \le\;& C\int_{\mathbb{R}}\phi^2 |(v^{S_1})_x|^2\,dx \\ &+ C\int_{\mathbb{R}}|v^C-v_*|^2 |(v^{S_1})_x|^2\,dx \\ &+ C\int_{\mathbb{R}}|v^{S_3}-v^*|^2 |(v^{S_1})_x|^2\,dx . \end{align}\]
For the perturbation term, since \(|(v^{S_1})_x|\lesssim \delta_1^2\) and \[\varphi_1+\varphi_3=1,\] we have \[\begin{align} \int_{\mathbb{R}}\phi^2 |(v^{S_1})_x|^2\,dx &\le C\delta_1^2\int_{\mathbb{R}}\phi^2 |(v^{S_1})_x|\,dx \\ &\le C\delta_1^2\int_{\mathbb{R}}|\varphi_1\phi|^2 |(v^{S_1})_x|\,dx + C\delta_1^2\int_{\mathbb{R}}|\varphi_3\phi|^2 |(v^{S_1})_x|\,dx . \end{align}\] By the definition of \(\mathcal{G}_1^S\) in ?? and Lemma 6, \[\begin{align} \int_{\mathbb{R}}\phi^2 |(v^{S_1})_x|^2\,dx \le C\delta_1^2\mathcal{G}_1^S + C\delta_1^4 e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U|\bar U)\,dx . \end{align}\]
Next, the interaction terms between the \(1\)-shock and the contact wave / \(3\)-shock are controlled by the previously established wave-interaction estimate (Lemma 7): \[\begin{align} &\int_{\mathbb{R}}|v^C-v_*|^2 |(v^{S_1})_x|^2\,dx + \int_{\mathbb{R}}|v^{S_3}-v^*|^2 |(v^{S_1})_x|^2\,dx\\ &\qquad \qquad \qquad \qquad \le C\delta_1^{3}\bigl(\delta_3^2e^{-C\delta_3 t}+(\delta_C^2+\delta_3^2)e^{-C\delta_1 t}\bigr). \end{align}\]
Combining the above bounds, we conclude that \[\begin{align} & \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|v-v^{S_1}\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \\ & \quad \le C\widetilde{\alpha}\delta_1^{2k+2}\mathcal{G}_1^S + C\widetilde{\alpha}\delta_1^{2k+4}e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U|\bar U)\,dx \\ &\qquad + C\widetilde{\alpha}\delta_1^{2k+3}\bigl(\delta_3^2e^{-C\delta_3 t}+(\delta_C^2+\delta_3^2)e^{-C\delta_1t}\bigr) + \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx . \end{align}\] This proves the lemma. ◻
Lemma 31. Let \(|\alpha|=1,2\). Assume that \[\bigl\lVert H\bigr\rVert_{\nu,M_\#} \le C\,\delta_1^{\,k}\,\bigl|(v^{S_1})_x\bigr|.\] Then \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|\partial_x^\alpha (v-v^{S_1})\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& C\delta_1^{2k+3} \bigl(\delta_3^{2(|\alpha|+1)}e^{-C\delta_3 t} +\delta_C^{2}e^{-Ct}\bigr) \\ &+ C\delta_1^{2k+2}\|\partial^\alpha\phi\|_{L^2_x}^2 + \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}}\bigl\lVert G\bigr\rVert_{M_\#}^2\,dx, \end{align}\] where \(\widetilde{\alpha}=O(1)\).
Proof. For convenience, we omit the shift \(X_1\). By Young’s inequality, for any \(\widetilde{\alpha}>0\), \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|\partial^\alpha_x (v-v^{S_1})\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& \widetilde{\alpha} \int_{\mathbb{R}} |\partial^\alpha_x (v-v^{S_1})|^2\bigl\lVert H\bigr\rVert_{M_\#}^2\,dx \\ &+ \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx . \end{align}\] Using the assumption on \(H\), we infer \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|\partial^\alpha_x (v-v^{S_1})\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& C\widetilde{\alpha}\,\delta_1^{2k} \int_{\mathbb{R}} |\partial^\alpha_x (v-v^{S_1})|^2\,|(v^{S_1})_x|^2\,dx \\ &+ \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx . \end{align}\]
We now decompose \[\partial_x^\alpha (v-v^{S_1}) = \partial_x^\alpha\phi + \partial_x^\alpha(v^C-v_*) + \partial_x^\alpha(v^{S_3}-v^*),\] and therefore \[\begin{align} \int_{\mathbb{R}} |\partial_x^\alpha (v-v^{S_1})|^2\,|(v^{S_1})_x|^2\,dx \le\;& C\int_{\mathbb{R}}|\partial_x^\alpha\phi|^2\,|(v^{S_1})_x|^2\,dx \\ &+ C\int_{\mathbb{R}}|\partial_x^\alpha(v^C-v_*)|^2\,|(v^{S_1})_x|^2\,dx \\ &+ C\int_{\mathbb{R}}|\partial_x^\alpha(v^{S_3}-v^*)|^2\,|(v^{S_1})_x|^2\,dx . \end{align}\]
For the perturbation term, since \(\|(v^{S_1})_x\|_{L^\infty_x}\le C\delta_1^2\), we obtain \[\begin{align} \int_{\mathbb{R}}|\partial_x^\alpha\phi|^2\,|(v^{S_1})_x|^2\,dx \le C\delta_1^2\|\partial_x^\alpha\phi\|_{L^2_x}^2. \end{align}\]
For the interaction terms involving the viscous contact wave and the \(3\)-shock profile, using the previously established derivative interaction bounds (Lemma 8), we derive that \[\begin{align} \int_{\mathbb{R}} |\partial_x^\alpha (v-v^{S_1})|^2\,|(v^{S_1})_x|^2\,dx \le\; C\delta_1^2\|\partial_x^\alpha\phi\|_{L^2_x}^2 + C\delta_1^{3} \bigl(\delta_3^{2(|\alpha|+1)}e^{-C\delta_3 t} +\delta_C^2e^{-C\delta_1t}\bigr). \end{align}\]
Substituting this estimate into the previous bound, we conclude that \[\begin{align} \iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|\partial_x^\alpha (v-v^{S_1})\bigr| \left|H\frac{G}{M_\#}\right|\,d\xi\,dx \le\;& C\delta_1^{2k+2}\|\partial^\alpha\phi\|_{L^2_x}^2 \\ &+ C\delta_1^{2k+3} \bigl(\delta_3^{2(|\alpha|+1)}e^{-C\delta_3 t} +\delta_C^{2}e^{-C\delta_1t}\bigr) \\ &+ \frac{1}{\widetilde{\alpha}} \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{M_\#}^2\,dx . \end{align}\] This proves the lemma. ◻
Lemma 32. Let \(|\beta|=0,1\). Assume that for \(j=0,1\), \[\bigl\lVert\partial_x^j H\bigr\rVert_{\nu,M_\#} \le C\,\delta_1^{k+j}\,\bigl|(v^{S_1})_x\bigr|.\] Then \[\begin{align} &\iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|\partial_x\bigl(v-(v^{S_1})^{-X_1}\bigr)\bigr| \, \bigl|\partial_x^\beta P_1(\xi_1H)\bigr| \, \Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx \\ &\le C(\delta_0+\varepsilon) \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\quad + C(\delta_0+\varepsilon)^{|\beta|}\delta_1^{k} \bigl( \delta_3^{2}\delta_1e^{-C\delta_3 t} +\delta_0^2\delta_1e^{-C\delta_1 t} \bigr) + C(\delta_0+\varepsilon)^{|\beta|}\delta_1^{k+1} \|\partial_x\phi\|_{L^2_x}^2 . \end{align}\]
Proof. For convenience, we omit the shift \(X_1\). We divide the proof into the cases \(|\beta|=0\) and \(|\beta|=1\).
Case 1: \(|\beta|=0\). Since \[P_1(\xi_1H) = \xi_1H-\sum_{j=0}^4\langle \xi_1H,\chi_j\rangle_M\chi_j,\] we write \[\begin{align} &\iint \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl|P_1(\xi_1H)\bigr| \, \Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx \\ &\le \iint \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl|\xi_1H\bigr| \, \Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx \\ &\qquad + C\iint \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \,\bigl|\langle \xi_1H,\chi_j\rangle_M\bigr| \,\bigl|M\bigr| \,\Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx =:I_1+I_2 . \end{align}\]
For \(I_1\), Holder’s inequality in \(\xi\) gives \[\begin{align} I_1 \le& \int \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl\lVert H\bigr\rVert_{\nu,M_\#} \, \bigl\lVert G\bigr\rVert_{\nu,M_\#} \, dx . \end{align}\] Using the assumption with \(j=0\), we obtain \[\begin{align} I_1 \le& C\delta_1^k \int \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl|(v^{S_1})_x\bigr| \, \bigl\lVert G\bigr\rVert_{\nu,M_\#} \, dx \\ \le& C\delta_1^{k-1} \int \bigl|\partial_x^\alpha(v-v^{S_1})\bigr|^2 \, \bigl|(v^{S_1})_x\bigr|^2\,dx + C\delta_1 \int \bigl\lVert G\bigr\rVert_{\nu,M_\#}^2 \,dx . \end{align}\] If \(|\alpha|=0\), we use the zeroth-order interaction estimate (Lemma 7); if \(|\alpha|=1\), we use the derivative interaction estimate (Lemma 8). In this case, \[\begin{align} I_1 \le& C\delta_1 \int \bigl\lVert G\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C\delta_1^{k+1} \bigl( \delta_1\delta_3^{4}e^{-C\delta_3 t} +\delta_C^2\delta_1e^{-C\delta_1t} \bigr) + C\delta_1^{k+1} \|\partial_x\phi\|_{L^2_x}^2 . \end{align}\] The term \(I_2\) is treated in exactly the same way, since \[|\langle \xi_1H,\chi_j\rangle_M| \le C\left( \int \frac{(1+|\xi|)|H|^2}{M_\#}\,d\xi \right)^{1/2}, \qquad \left|\frac{M}{M_\#}\right|\le C.\] This proves the estimate for \(|\beta|=0\). Also, we can compute this for \(|\alpha|=0\). That is,
\[\begin{align} \label{eq:kc3-1} &\iint_{\mathbb{R}\times\mathbb{R}^3} \bigl|v-(v^{S_1})^{-X_1}\bigr| \, \bigl|\partial_x^\beta P_1(\xi_1H)\bigr| \, \Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx \nonumber \\ &\le C\delta_1 \int_{\mathbb{R}} \bigl\lVert G\bigr\rVert_{\nu,M_\#}^2\,dx + C\delta_1^{k+1} \bigl( \delta_3^{4}\delta_1e^{-C\delta_3 t} +\delta_0^2\delta_1e^{-C\delta_1 t} \bigr) \nonumber \\ &\quad +C\delta_1^{k+1}\mathcal{G}_1^S + C\delta_1^{k+3} e^{-C\delta_1 t}\int_{\mathbb{R}}\eta(U|\bar U)\,dx . \end{align}\tag{137}\]
Case 2: \(|\beta|=1\). Differentiating the projection gives \[\partial_x P_1(\xi_1H) = \xi_1H_x - \sum_{j=0}^4 \Bigl( \partial_x\langle \xi_1H,\chi_j\rangle_M\,\chi_j + \langle \xi_1H,\chi_j\rangle_M\,\partial_x\chi_j \Bigr).\] Hence \[\begin{align} \left|\partial_x P_1(\xi_1H)\right| \le& |\xi_1H_x| + C|(v_x,u_x,\theta_x)|\,|M| \, \bigl\lVert H\bigr\rVert_{\nu,M_\#} + C|M|\,\bigl\lVert H_x\bigr\rVert_{\nu,M_\#}. \end{align}\] Accordingly, \[\begin{align} &\iint \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl|\partial_xP_1(\xi_1H)\bigr| \, \Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx \\ &\le \iint \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \,\bigl|\xi_1H_x\bigr| \, \Bigl|\frac{G}{M_\#}\Bigr|\,d\xi\,dx \\ &\qquad + C\iint \bigl|(v_x,u_x,\theta_x)\bigr|\, \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl\lVert H\bigr\rVert_{\nu,M_\#} \, \Bigl|\frac{MG}{M_\#}\Bigr|\,d\xi\,dx \\ &\qquad + C\iint \bigl|\partial_x^\alpha(v-v^{S_1})\bigr| \, \bigl\lVert H_x\bigr\rVert_{\nu,M_\#} \, \Bigl|\frac{MG}{M_\#}\Bigr|\,d\xi\,dx =:J_1+J_2+J_3 . \end{align}\]
Using the assumptions with \(j=0,1\), together with the a priori bound \[\|(v_x,u_x,\theta_x)\|_{L^\infty_x}\le C(\delta_0+\varepsilon),\] we estimate each \(J_\ell\) exactly as above and obtain \[\begin{align} J_\ell \le& C(\delta_0+\varepsilon) \int \bigl\lVert G\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C(\delta_0+\varepsilon)\delta_1^{k} \bigl( \delta_1\delta_3^{|\alpha|+2}e^{-C\delta_3 t} +\delta_0^2\delta_1^{|\alpha|+1}e^{-C\delta_1 t} \bigr) \\ &\qquad + C(\delta_0+\varepsilon)\delta_1^{k+2} \|\partial^\alpha\phi\|_{L^2_x}^2 , \qquad \ell=1,2,3. \end{align}\] Summing these bounds gives the desired estimate for \(|\beta|=1\), and the proof is complete. ◻
The next lemma gives the differentiated source estimate needed in the high-order microscopic analysis.
Lemma 33. There exists a constant \(C>0\) such that \[\begin{align} & \iint_{\mathbb{R}\times\mathbb{R}^3} \partial_x \left[ -\frac{1}{v}P_1(\xi_1M_x) +\sum_{i=1,3}\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}P_1^{S_i}\left(\xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}\right) \right] \frac{|G|}{M_\#}\,d\xi\,dx \\ &\leq C\widetilde{\alpha}(\delta_0+\varepsilon)^2\bigl\lVert\left(\phi_x,\psi_x,\zeta_x\right)\bigr\rVert_{L^2}^2 + C\widetilde{\alpha}\delta_0^3(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}) + C\widetilde{\alpha}\frac{\delta_C^4}{(1+t)^{3/2}} \\ &\quad + C\widetilde{\alpha}(\varepsilon+\delta_0)^2\delta_3^2 e^{-C\delta_3t} + C\widetilde{\alpha}(\varepsilon+\delta_0)^2\delta_1^2 e^{-C\delta_1t} + \frac{1}{\widetilde{\alpha}}\int_{\mathbb{R}}\bigl\lVert G\bigr\rVert_{M_\#}^2 \,dx \\ &\quad + C\widetilde{\alpha}\bigl\lVert\left(\psi_{xx},\zeta_{xx}\right)\bigr\rVert_{L^2}^2 + C\widetilde{\alpha}(\delta_0+\varepsilon)^2 (\mathcal{G}_1^S+\mathcal{G}_3^S), \end{align}\] where \(\widetilde{\alpha}=O(1)\).
Proof. Set \[\mathfrak R := -\frac{1}{v}P_1(\xi_1M_x) +\sum_{i=1,3}\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}P_1^{S_i}\Bigl(\xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}} \Bigr) .\] We only prove the case \(|\alpha|=1\). We first decompose the Maxwellian part: \[\begin{align} &-\frac{1}{v}\xi_1 M_x + \sum_{i=1,3}\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\xi_1 \partial_x \bigl(M^{S_{i}}\bigr)^{-X_{i}} \\ &\quad = -\frac{1}{v}\xi_1 \left(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\right)_x +\sum_{i=1,3}\left(\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}-\frac{1}{v}\right)\xi_1 \partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}, \end{align}\] and similarly for the projected part, \[\begin{align} &-\frac{1}{v}\langle \xi_1 M_x, M\rangle_M\chi + \sum_{i=1,3} \frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\bigl\langle \xi_1 \partial_x \bigl(M^{S_{i}}\bigr)^{-X_{i}}, \bigl(\chi^{S_{i}}\bigr)^{-X_{i}}\bigr\rangle_{S_i}\bigl(\chi^{S_{i}}\bigr)^{-X_{i}}\\ &\qquad = -\frac{1}{v}\bigl\langle \xi_1 \left(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\right)_x , \chi \bigr\rangle_M \chi \\ &\qquad \quad + \sum_{i=1,3} \left(\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}-\frac{1}{v}\right)\bigl\langle \xi_1 \partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}, \chi \bigr\rangle_M \chi\\ &\qquad \quad + \sum_{i=1,3} \frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}} \Biggl\{\bigl\langle \xi_1 \partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}, \bigl(\chi^{S_{i}}\bigr)^{-X_{i}} \bigr\rangle_{S_i}\bigl(\chi^{S_{i}}\bigr)^{-X_{i}} \Biggr. \\ &\qquad \qquad \qquad \qquad \qquad \qquad \qquad \qquad \Biggl.-\bigl\langle \xi_1 \partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}, \chi \bigr\rangle_M\chi\Biggr\}. \end{align}\] Accordingly, we write \[\mathfrak R=\sum_{j=1}^5 \mathcal{K}_j,\] where \[\begin{align} \mathcal{K}_1 :=& \iint \left\{-\frac{1}{v}\xi_1\left(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\right)_x\right\}\frac{|G|}{M_\#} \,d\xi dx,\\ \mathcal{K}_{2i} :=& \iint \left(\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}-\frac{1}{v}\right)\xi_1 \partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}} \frac{|G|}{M_\#} \,d\xi dx,\qquad (i=1,3),\\ \mathcal{K}_{3} :=& -\iint \frac{1}{v} \Bigl\langle \xi_1\left(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\right)_x ,\chi \Bigr\rangle_M \chi \frac{|G|}{M_\#} \,d\xi dx,\\ \mathcal{K}_{4i} :=& \iint \left(\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}-\frac{1}{v}\right)\Bigl\langle \xi_1 \partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}, \chi \Bigr\rangle_M \chi \frac{|G|}{M_\#} \,d\xi dx,\qquad (i=1,3),\\ \mathcal{K}_{5i} :=& \iint \frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}} \Bigl\{\Bigl\langle \xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}},\bigl(\chi^{S_{i}}\bigr)^{-X_{i}} \Bigr\rangle_{S_i}\bigl(\chi^{S_{i}}\bigr)^{-X_{i}} \\ & \qquad \qquad \qquad \qquad -\Bigl\langle \xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}},\chi \Bigr\rangle_M \chi\Bigr\} \frac{|G|}{M_\#} \,d\xi dx,\qquad (i=1,3), \end{align}\] and \(\mathcal{K}_j:=\mathcal{K}_{j1}+\mathcal{K}_{j3}\) for \(j=2,4,5\). Using Young’s inequality and the smooth dependence of \(M\) and \(\chi\) on the macroscopic variables, it suffices to estimate the differentiated forms of the representative terms \[\mathcal{H}_1,\;\mathcal{H}_2,\;\mathcal{H}_{3i},\;\mathcal{H}_{4i},\;\mathcal{H}_{5i},\] defined by \[\begin{align} \mathcal{H}_1 := & \iint \Bigl|P_1\xi_1\partial_{xx} \Bigl(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\Bigr) \Bigr|\,\Bigl|\frac{G}{M_\#} \Bigr| \,d\xi\, dx, \\ \mathcal{H}_2 := & \iint |v_x| \, \Bigl|\xi_1\Bigl(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\Bigr)_x\Bigr|\, \Bigl|\frac{G}{M_\#}\Bigr| \,d\xi \, dx, \\ \mathcal{H}_{3i} := & \iint \Bigl|v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr|\, \Bigl|\xi_1\partial_{xx}\bigl(M^{S_{i}}\bigr)^{-X_{i}}\Bigr| \, \Bigl|\frac{G}{M_\#}\Bigr| \,d\xi \, dx,\qquad (i=1,3), \\ \mathcal{H}_{4i} := & \iint \Bigl|\Bigl(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr)_x\Bigr|\,\Bigl|\xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}\Bigr|\,\Bigl|\frac{G}{M_\#}\Bigr| \,d\xi \, dx,\qquad (i=1,3), \\ \mathcal{H}_{5i} := & \iint |v_x| \, \Bigl|v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr|\, \Bigl|\xi_1\partial_x\bigl(M^{S_{i}}\bigr)^{-X_{i}}\Bigr| \, \Bigl|\frac{G}{M_\#}\Bigr| \,d\xi \, dx,\qquad (i=1,3). \end{align}\] \(\mathcal{H}_1\) comes from \(\mathcal{K}_1+\mathcal{K}_3\). We only spell out the estimate of \(\mathcal{H}_2\), since the others are handled in the same way by Lemmas 30–32, the derivative wave-interaction estimate, and the standard decay bounds for the composite wave. By the cutoff decomposition, \[\begin{align} &\Bigl|\Bigl(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\Bigr)_x\Bigr| \\ &\quad \leq \varphi_1\Bigl|\Bigl(M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}\Bigr)_x\Bigr| +\varphi_3\Bigl|\Bigl(M-\bigl(M^{S_{3}}\bigr)^{-X_{3}}\Bigr)_x\Bigr| +C\varphi_3 \Bigl|\bigl(M^{S_{1}}\bigr)^{-X_{1}}\,\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\Bigr| \\ &\qquad +C \varphi_1 \Bigl|\bigl(M^{S_{3}}\bigr)^{-X_{3}} \, \partial_x\bigl(v^{S_{3}}\bigr)^{-X_{3}}\Bigr|, \end{align}\] and therefore \[\begin{align} \mathcal{H}_2 \leq\;& \frac{1}{\widetilde{\alpha}}\iint \frac{|G|^2}{M_\#} \,d\xi dx + C\widetilde{\alpha}\sum_{i=1,3} \Biggl\{ \int \varphi_i^2|v_x|^2 \, \Bigl|\Bigl(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr)_x\Bigr|^2 \,dx \Biggr.\\ &\qquad \qquad \qquad \qquad \qquad \qquad \quad \Biggl.+ \int (1-\varphi_i)^2 |v_x|^2\, \Bigl|\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\Bigr|^2 \,dx \Biggr\}. \end{align}\] For \(i=1\), we decompose \[v_x-\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}} = \phi_x+\bigl(v^C-v_*\bigr)_x+\bigl(\bigl(v^{S_{3}}\bigr)^{-X_{3}}-v^*\bigr)_x\] and obtain \[\begin{align} &\int \varphi_1^2 |v_x|^2 \, \Bigl|\Bigl(v-\bigl(v^{S_{1}}\bigr)^{-X_{1}}\Bigr)_x\Bigr|^2 dx \\ & \qquad \le C(\delta_0+\varepsilon)^2 \|\phi_x\|_{L^2}^2 + C\delta_0^3(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t})+ C\int |v_x^C|^4 \,dx \\ & \qquad \qquad + C(\varepsilon+\delta_0)^2\int \varphi_1^2 \, \Bigl|\partial_x\bigl(v^{S_{3}}\bigr)^{-X_{3}}\Bigr|^2 \,dx. \end{align}\] Since \[\int |v_x^C|^4 \,dx \le C\frac{\delta_C^4}{(1+t)^{3/2}}, \qquad \int \varphi_1^2 \Bigl|\partial_x\bigl(v^{S_{3}}\bigr)^{-X_{3}}\Bigr|^2 \,dx \le C\delta_3^2 e^{-C\delta_3t},\] it follows that \[\begin{align} \mathcal{H}_2 \leq\;& \frac{1}{\widetilde{\alpha}}\int \bigl\lVert G\bigr\rVert_{M_\#}^2 \,dx + C\widetilde{\alpha}(\delta_0+\varepsilon)^2\|\phi_x\|_{L^2}^2 + C\widetilde{\alpha}\delta_0^3(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t})\\ &+ C\widetilde{\alpha}\frac{\delta_C^4}{(1+t)^{3/2}} + C\widetilde{\alpha}(\varepsilon+\delta_0)^2\delta_3^2 e^{-C\delta_3t}. \end{align}\] The term \(\mathcal{H}_1\) can be treated in the same way as \(\mathcal{H}_2\). The key point is that the microscopic projection eliminates the leading density contribution, so no \(\phi_{xx}\)-term appears in the estimate. The remaining terms \(\mathcal{H}_{3i}\), \(\mathcal{H}_{4i}\), and \(\mathcal{H}_{5i}\), together with the differentiated projector-mismatch terms arising from \(\mathcal{K}_3\), \(\mathcal{K}_{4i}\), and \(\mathcal{K}_{5i}\), are estimated by the same combination of Young’s inequality, the smooth dependence of \(M\) and \(\chi\) on the macroscopic variables, Lemmas 30–32, and the derivative interaction bounds. Summing all these contributions gives the stated inequality. ◻
Remark 2. The above estimate is formulated only for \(|\alpha|=1\). The reason is that the corresponding undifferentiated argument (\(\alpha=0\)) does not close at the zeroth-order level because of the contact-wave contribution. Indeed, \[\int \varphi_1^2 |v_x^C|^2 \,dx \le C\frac{\delta_C}{1+t}\int_{-\infty}^{\sigma_1 t/4} e^{-c x^2/(1+t)}\,dx,\] and the right-hand side is not globally time-integrable. By contrast, \[\int \varphi_1^2 |v_{xx}^C|^2 \,dx \le C\frac{\delta_C}{(1+t)^2}\int_{-\infty}^{\sigma_1 t/4} e^{-c x^2/(1+t)}\,dx \le C\frac{\delta_C}{(1+t)^{3/2}},\] which is integrable in time. This explains why the contact contribution must be excluded from the zeroth-order argument and why the differentiated estimate \(|\alpha|=1\) is the relevant form used in the high-order microscopic analysis.
Lemma 34. Let \(P(\xi)\) be a fixed polynomial in \(\xi\), and assume that \(g\in \mathfrak Z^\perp\), so that \(L_M^{-1}g\) is well-defined. Then \[\begin{align} \label{eq:kc5} \left( \int_{\mathbb{R}^3_\xi} P(\xi)\,(L_M^{-1}g)_x\,d\xi \right)^2 \le\;& \frac{C}{\lambda_{\mathrm{mic}}^{2}} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g_x|^2}{M_\#}\,d\xi \\ &+ \frac{C}{\lambda_{\mathrm{mic}}^{4}} \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)|M_x|^2}{M_\#}\,d\xi \right) \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g|^2}{M_\#}\,d\xi \right). \nonumber \end{align}\qquad{(41)}\]
Proof. Since \(P(\xi)\) is a fixed polynomial and \(M_\#\) is a global Maxwellian, we have \[\left( \int_{\mathbb{R}^3_\xi} P(\xi)\,(L_M^{-1}g)_x\,d\xi \right)^2 \le C \int_{\mathbb{R}^3_\xi} \frac{|(L_M^{-1}g)_x|^2}{M_\#}\,d\xi .\] Next, by differentiating the identity \(L_M(L_M^{-1}g)=g\), we obtain \[(L_M^{-1}g)_x = L_M^{-1}(g_x) - L_M^{-1}\Bigl( \mathcal{N}(M_x,L_M^{-1}g)+\mathcal{N}(L_M^{-1}g,M_x) \Bigr).\] Therefore, \[\begin{align} \int_{\mathbb{R}^3_\xi} \frac{|(L_M^{-1}g)_x|^2}{M_\#}\,d\xi \le\;& C \int_{\mathbb{R}^3_\xi} \frac{|L_M^{-1}g_x|^2}{M_\#}\,d\xi \\ &+ C \int_{\mathbb{R}^3_\xi} \frac{\bigl|L_M^{-1}(\mathcal{N}(M_x,L_M^{-1}g)+\mathcal{N}(L_M^{-1}g,M_x))\bigr|^2}{M_\#}\,d\xi . \end{align}\] By the standard weighted estimate for \(L_M^{-1}\), \[\int_{\mathbb{R}^3_\xi} \frac{|L_M^{-1}h|^2}{M_\#}\,d\xi \le \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|h|^2}{M_\#}\,d\xi ,\] we obtain \[\begin{align} \int_{\mathbb{R}^3_\xi} \frac{|(L_M^{-1}g)_x|^2}{M_\#}\,d\xi \le\;& \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g_x|^2}{M_\#}\,d\xi \\ &+ \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|\mathcal{N}(M_x,L_M^{-1}g)|^2}{M_\#}\,d\xi \\ &+ \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|\mathcal{N}(L_M^{-1}g,M_x)|^2}{M_\#}\,d\xi . \end{align}\] Using the standard bilinear estimate for the collision operator, \[\int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|\mathcal{N}(f,h)|^2}{M_\#}\,d\xi \le C \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)|f|^2}{M_\#}\,d\xi \right) \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|h|^2}{M_\#}\,d\xi \right),\] with \((f,h)=(M_x,L_M^{-1}g)\) and \((L_M^{-1}g,M_x)\), we deduce \[\begin{align} \int_{\mathbb{R}^3_\xi} \frac{|(L_M^{-1}g)_x|^2}{M_\#}\,d\xi \le\;& \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g_x|^2}{M_\#}\,d\xi \\ &+ \frac{C}{\lambda_{\mathrm{mic}}^2} \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)|M_x|^2}{M_\#}\,d\xi \right) \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|L_M^{-1}g|^2}{M_\#}\,d\xi \right). \end{align}\] Applying once again the weighted estimate for \(L_M^{-1}\), \[\int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|L_M^{-1}g|^2}{M_\#}\,d\xi \le \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g|^2}{M_\#}\,d\xi ,\] we conclude that \[\begin{align} \int_{\mathbb{R}^3_\xi} \frac{|(L_M^{-1}g)_x|^2}{M_\#}\,d\xi \le\;& \frac{C}{\lambda_{\mathrm{mic}}^2} \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g_x|^2}{M_\#}\,d\xi \\ &+ \frac{C}{\lambda_{\mathrm{mic}}^4} \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)|M_x|^2}{M_\#}\,d\xi \right) \left( \int_{\mathbb{R}^3_\xi} \frac{(1+|\xi|)^{-1}|g|^2}{M_\#}\,d\xi \right). \end{align}\] Combining this with the first inequality proves ?? . ◻
Lemma 35. Let \(P(\xi)\) be a fixed polynomial in \(\xi\). Recall that \(\widetilde{\Pi}_1\) is defined by 97 . \[\begin{align} \label{eq:kc6} \begin{aligned} &\int_{\mathbb{R}} \left( \int_{\mathbb{R}^3_\xi} P(\xi)\,\partial_x \widetilde{\Pi}_1 \,d\xi \right)^2 dx\\ \le\;& C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i \mathcal{G}^S_i + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i |\dot{X}_i|^2 + C(\delta_0+\varepsilon)\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2_x}^2\\ &+ C(\delta_0+\varepsilon) \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 dx \\ &+ C \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\delta_0^2\left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) \\ & + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}}. \end{aligned} \end{align}\qquad{(42)}\]
Proof. Recall that \[\widetilde{\Pi}_1 := \Pi_1-\bigl((\Pi_1^{S_{1}})^{-X_{1}}\bigr)-\bigl((\Pi_1^{S_{3}})^{-X_{3}}\bigr).\] By Young’s inequality in \(\xi\), \[\begin{align} \label{eq:kc6-reduce} \int_{\mathbb{R}} \left( \int_{\mathbb{R}^3_\xi} P(\xi)\,\widetilde{\Pi}_{1x}\,d\xi \right)^2 dx \le C \iint_{\mathbb{R}\times\mathbb{R}^3} \frac{|\widetilde{\Pi}_{1x}|^2}{M_\#}\,d\xi\,dx . \end{align}\tag{138}\] Recall the decomposition \[\begin{align} \widetilde{\Pi}_1 =&\; L_M^{-1}P_1\Biggl[\widetilde{G}_t-\frac{u_1}{v}\widetilde{G}_x+\frac{1}{v}P_1\Bigl(\xi_1\widetilde{G}_x\Bigr)-\mathcal{N}\Bigl(\widetilde{G},\widetilde{G}\Bigr)\Biggr] \\ &\; -L_M^{-1}\Biggl[\mathcal{N}\Bigl(\widetilde{G},\bigl(G^{S_{1}}\bigr)^{-X_{1}}+\bigl(G^{S_{3}}\bigr)^{-X_{3}}\Bigr)+\mathcal{N}\Bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}}+\bigl(G^{S_{3}}\bigr)^{-X_{3}},\widetilde{G}\Bigr)\Biggr] \\ &\; +L_M^{-1}\Biggl[\mathcal{N}\Bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(G^{S_{3}}\bigr)^{-X_{3}}\Bigr)+\mathcal{N}\Bigl(\bigl(G^{S_{3}}\bigr)^{-X_{3}},\bigl(G^{S_{1}}\bigr)^{-X_{1}}\Bigr)\Biggr] \\ &\; -\dot{X}_1\bigl(L_{1}^S\bigr)^{-1}\Bigl(\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\Bigr) -\dot{X}_3\bigl(L_{3}^S\bigr)^{-1}\Bigl(\partial_x\bigl((G^{S_{3}})^{-X_{3}}\bigr)\Bigr) +J, \end{align}\] where \[\begin{align} J :=&\; \sum_{i\in\{1,3\}} \Bigl(L_M^{-1}P_1-\bigl(L_{i}^S\bigr)^{-1}P_1^{S_i}\Bigr) \Bigl[\partial_t\bigl(G^{S_{i}}\bigr)^{-X_{i}}-\mathcal{N}\Bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\Bigr)\Bigr] \\ &+ \sum_{i\in\{1,3\}} \Biggl[\frac{\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\bigl(L_{i}^S\bigr)^{-1}P_1^{S_i}-\frac{u_1}{v}L_M^{-1}P_1\Biggr] \Bigl(\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\Bigr) \\ &+ \sum_{i\in\{1,3\}} \Biggl[\frac{1}{v}L_M^{-1}P_1\xi_1-\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\bigl(L_{i}^S\bigr)^{-1}P_1^{S_i}\xi_1\Biggr] \Bigl(\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\Bigr), \end{align}\] and \(L_{i}^{S}:=L_{\bigl(M^{S_{i}}\bigr)^{-X_{i}}}\). Accordingly, write \[\widetilde{\Pi}_1=\mathcal{P}^{(1)}+\mathcal{P}^{(2)}+\mathcal{P}^{(3)}+\mathcal{P}^{(4)}+\mathcal{P}^{(5)},\] where the five pieces correspond to the five displayed lines above. We estimate each contribution to \(\iint |\mathcal{P}_x|^2/M_\#\). Step 1: the main microscopic terms \(\mathcal{P}^{(1)}\). Applying Lemma 34 to \[g=\widetilde{G}_t-\frac{u_1}{v}\widetilde{G}_x+\frac{1}{v}P_1(\xi_1\widetilde{G}_x)-\mathcal{N}(\widetilde{G},\widetilde{G}),\] we obtain \[\begin{align} \label{eq:kc6-P1} \iint \frac{|(\mathcal{P}^{(1)})_x|^2}{M_\#}\,d\xi\,dx \le\;& C \iint \frac{(1+|\xi|)^{-1}|g_x|^2}{M_\#}\,d\xi\,dx \\ &+ C(\delta_0+\varepsilon) \iint \frac{(1+|\xi|)^{-1}|g|^2}{M_\#}\,d\xi\,dx . \nonumber \end{align}\tag{139}\] Using the product rule and the a priori smallness of \((v_x,u_x,\theta_x)\), we have \[\begin{align} |g_x| \le\;& |\widetilde{G}_{tx}| + C(\delta_0+\varepsilon)|\widetilde{G}_x| + C|\widetilde{G}_{xx}| + C(\delta_0+\varepsilon)|\widetilde{G}_t| \\ &+ C\,|\mathcal{N}(\widetilde{G},\widetilde{G})_x|, \end{align}\] and similarly for \(g\). By the standard bilinear collision estimate and the bootstrap smallness, \[\iint \frac{(1+|\xi|)^{-1}|\mathcal{N}(\widetilde{G},\widetilde{G})_x|^2}{M_\#}\,d\xi\,dx \le C(\delta_0+\varepsilon) \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_{\text{x}}\bigr\rVert_{\nu,M_\#}^2\,dx .\] Therefore, \[\begin{align} \label{eq:kc6-P1-final} \iint \frac{|(\mathcal{P}^{(1)})_x|^2}{M_\#}\,d\xi\,dx \le\;& C \int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C(\delta_0+\varepsilon) \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2\,dx . \nonumber \end{align}\tag{140}\] Step 2: the mixed collision terms \(\mathcal{P}^{(2)}\). Using again Lemma 34, together with the standard bilinear estimate for \(\mathcal{N}\bigl(\widetilde{G},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\) and \(\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}\bigr)\), we obtain \[\begin{align} \label{eq:kc6-P2-final} \iint \frac{|(\mathcal{P}^{(2)})_x|^2}{M_\#}\,d\xi\,dx \le\;& C(\delta_0+\varepsilon) \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C(\delta_0+\varepsilon)^2\delta_0^3\left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) . \nonumber \end{align}\tag{141}\] Step 3: the shock–shock interaction terms \(\mathcal{P}^{(3)}\). Since \(\bigl(G^{S_{1}}\bigr)^{-X_{1}}\) and \(\bigl(G^{S_{3}}\bigr)^{-X_{3}}\) are exponentially localized and spatially separated, \[\begin{align} \label{eq:kc6-P3-final} \iint \frac{|(\mathcal{P}^{(3)})_x|^2}{M_\#}\,d\xi\,dx \le C(\delta_0+\varepsilon)^2\delta_0^3 \left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) . \end{align}\tag{142}\] Step 4: the shift terms \(\mathcal{P}^{(4)}\). By the explicit profile bounds, \[\iint \frac{\bigl|\partial_x\bigl(\bigl(L_{i}^S\bigr)^{-1}\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\bigr|^2}{M_\#}\,d\xi\,dx \le C\delta_i^2, \qquad i=1,3.\] Hence \[\begin{align} \label{eq:kc6-P4-final} \iint \frac{|(\mathcal{P}^{(4)})_x|^2}{M_\#}\,d\xi\,dx \le C\sum_{i=1,3}\delta_i^2|\dot{X}_i|^2 \le C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 . \end{align}\tag{143}\] Step 5: the coefficient-mismatch terms \(J=\mathcal{P}^{(5)}\). These are the most delicate terms. We only record representative estimates; the remaining variants are treated in the same way. First, for the difference of inverse linearized operators, \[\begin{align} \Bigl(L_M^{-1}-\bigl(L_{1}^S\bigr)^{-1} \Bigr) \bigl(\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr) =\; & L_M^{-1}\Bigl( \mathcal{N}\bigl(\bigl(M^{S_{1}}\bigr)^{-X_{1}}-M,\bigl(L_{1}^S\bigr)^{-1}\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr) \\ & + \mathcal{N}\bigl(\bigl(L_{1}^S\bigr)^{-1}\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(M^{S_{1}}\bigr)^{-X_{1}}-M\bigr) \Bigr), \end{align}\] and Lemma 34 gives \[\begin{align} & \iint \frac{\Bigl|\partial_x\Bigl\{\bigl(L^{-1}_M-\bigl(L_{1}^S\bigr)^{-1}\bigr)\bigl(\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr)\Bigr\}\Bigr|^2}{M_\#}\,d\xi\,dx \\ & \quad \le C(\delta_0+\varepsilon)^2\int \bigl|\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\bigr|^2 \, \bigl|\bigl(v-\bigl(v^{S_{1}}\bigr)^{-X_{1}} \bigr)_x\bigr|^2\,dx \\ & \quad \qquad + C(\delta_0+\varepsilon)^2\int \bigl|\partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\bigr|^2 \, \bigl|v-\bigl(v^{S_{1}}\bigr)^{-X_{1}}\bigr|^2\,dx . \end{align}\] By Lemmas 30–33, this is bounded by \[\begin{align} \label{eq:kc6-J1} C(\delta_0+\varepsilon)^2\delta_1\mathcal{G}_1^S + C(\delta_0+\varepsilon)^2\delta_0^3\left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) + C(\delta_0+\varepsilon)^2\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2_x}^2 . \end{align}\tag{144}\] Next, for the coefficient mismatch \[\begin{align} & \frac{\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}}\bigl(L_{1}^S\bigr)^{-1}-\frac{u_1}{v}L^{-1}_M \\ &\quad = \frac{\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}-u_1}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}}\bigl(L_{1}^{S}\bigr)^{-1} -\frac{u_1}{v\bigl(v^{S_{1}}\bigr)^{-X_{1}}}\bigl(\bigl(v^{S_{1}}\bigr)^{-X_{1}}-v\bigr)\bigl(L_{1}^S\bigr)^{-1} +\frac{u_1}{v}\bigl(\bigl(L^{S}_{1}\bigr)^{-1}-L^{-1}_M\bigr), \end{align}\] each term is treated exactly as above, giving \[\begin{align} \label{eq:kc6-J2} C(\delta_0+\varepsilon)^2\delta_1\mathcal{G}_1^S + C(\delta_0+\varepsilon)^2\delta_0^3\left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) + C(\delta_0+\varepsilon)^2\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2_x}^2 . \end{align}\tag{145}\] Finally, for the projector mismatch terms, for example \[\begin{align} & \frac{1}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}} L_M^{-1} \Biggl[\Bigl\langle \xi_1\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},\chi_j-\bigl(\chi_j^{S_{1}}\bigr)^{-X_{1}} \Bigr\rangle_M \chi_j\Biggr], \\ & \frac{1}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}} L_M^{-1} \Biggl[\Bigl\langle \xi_1\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(\chi_j^{S_{1}}\bigr)^{-X_{1}} \Bigr\rangle_{S_1}\Bigl(\chi_j-\bigl(\chi_j^{S_{1}}\bigr)^{-X_{1}}\Bigr)\Biggr], \end{align}\] we use the smooth dependence of \(\chi_j\) on the macroscopic variables and Lemma 34 to obtain \[\begin{align} \label{eq:kc6-J3} C(\delta_0+\varepsilon)^2\delta_1\mathcal{G}_1^S + C(\delta_0+\varepsilon)^2\delta_0^3\left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) + C(\delta_0+\varepsilon)^2\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2_x}^2 . \end{align}\tag{146}\] The analogous \(i=3\) terms satisfy the same bounds. Therefore, \[\begin{align} \label{eq:kc6-P5-final} \iint \frac{|(\mathcal{P}^{(5)})_x|^2}{M_\#}\,d\xi\,dx \le\;& C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i \mathcal{G}_i^S + C(\delta_0+\varepsilon)\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)^2\delta_0^3\left(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\right) + C \frac{\delta_C}{(1+t)^\frac{5}{4}}. \nonumber \end{align}\tag{147}\] Combining 138 , 140 , 141 , 142 , 143 , and 147 , we obtain ?? . ◻
We point out that some intermediate estimates are not closed at each fixed derivative level. For instance, the estimate of \(\widetilde{G}_x\) contains higher-order terms such as \(\widetilde{G}_{xx}\) on the right hand side. This does not lead to a loss of derivatives, since the high-order energy estimate is closed simultaneously over all relevant derivative levels. More precisely, the terms involving \(\widetilde{G}_{xx}\) are controlled by the dissipation part of the final high-order energy functional, after summing the estimates for different derivative orders with suitable weights. Therefore, the estimate for \(\widetilde{G}_x\) should be understood as one component of the couple high-order energy argument rather than as an independent closed estimate.
Lemma 36. There exists a constant \(C>0\) such that \[\begin{align} \begin{aligned} &\frac{d}{dt}\iint_{\mathbb{R}}\bigl\lVert\widetilde{G}_{x}\bigr\rVert^2_{M_\#} \,dx +\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\le C(\delta_0+\varepsilon)\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 +C\delta_0^2(\delta_0+\varepsilon)\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) +C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} \\ &\quad +C\|(\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 +C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 +C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) \\ &\quad +C(\delta_0+\varepsilon)\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx +C\int_\mathbb{R} \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 dx. \end{aligned} \end{align}\]
Proof. Differentiate 37 with respect to \(x\), multiply the resulting equation by \(\widetilde{G}_x/M_\#\), and integrate over \((x,\xi)\in\mathbb{R}\times\mathbb{R}^3\). Then \[\begin{align} \frac{1}{2}\frac{d}{dt}\iint \frac{|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx = \mathcal{T}_1+\sum_{i=1,3}\mathcal{T}_{2i} +\mathcal{T}_3+\sum_{i=1,3}\mathcal{T}_{4i} +\sum_{i=1,3}\mathcal{T}_{5i} +\mathcal{T}_6+\mathcal{T}_7+\mathcal{T}_8+\mathcal{T}_9+\mathcal{T}_{10}, \end{align}\] where \[\begin{align} \mathcal{T}_1 &:= \iint (L_M\widetilde{G})_x\,\frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{2i} &:= \iint \dot{X}_i\,\bigl(\partial_{xx}\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\,\frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_3 &:= \iint \left(\frac{u_1}{v}\widetilde{G}_x-\frac{1}{v}P_1(\xi_1\widetilde{G}_x)\right)_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{4i} &:= \iint \Biggl[ \left(\frac{u_1}{v}-\frac{\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\right)\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}} \Biggr]_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{5i} &:= -\iint \Biggl[ \frac{1}{v}P_1(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}) -\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\bigl(P_1^{S_i}\bigr)(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}) \Biggr]_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_6 &:= \iint \Biggl[ -\frac{1}{v}P_1(\xi_1M_x) +\frac{1}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}}\bigl(P_1^{S_1}\bigr)(\xi_1\partial_x\bigl(M^{S_{1}}\bigr)^{-X_{1}})\Biggr.\\ &\qquad \qquad \Biggl. +\frac{1}{\bigl(v^{S_{3}}\bigr)^{-X_{3}}}\bigl(P_1^{S_3}\bigr)(\xi_1\partial_x\bigl(M^{S_{3}}\bigr)^{-X_{3}}) \Biggr]_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_7 &:= \iint \bigl(\mathcal{N}(\widetilde{G},\widetilde{G})\bigr)_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_8 &:= \sum_{i=1,3}\iint \Bigl[\mathcal{N}\bigl(\widetilde{G},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)+\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}\bigr)\Bigr]_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_9 &:= \iint \Bigl[\mathcal{N}\bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(G^{S_{3}}\bigr)^{-X_{3}}\bigr)+\mathcal{N}\bigl(\bigl(G^{S_{3}}\bigr)^{-X_{3}},\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr)\Bigr]_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{10} &:= \sum_{i=1,3}\iint \Bigl[(L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}}\Bigr]_x \frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx. \end{align}\]
We estimate these terms one by one.
1. Estimate of \(\mathcal{T}_1\). Since \[L_M h=\mathcal{N}(M,h)+\mathcal{N}(h,M),\] we have \[\label{eq:GxE-LM-diff} (L_Mh)_x=L_Mh_x+\mathcal{N}(M_x,h)+\mathcal{N}(h,M_x).\tag{148}\] Hence \[\begin{align} \mathcal{T}_1 &= \iint L_M\widetilde{G}_x\,\frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx +\iint \Bigl(\mathcal{N}(M_x,\widetilde{G})+\mathcal{N}(\widetilde{G},M_x)\Bigr)\frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx . \end{align}\] By Lemma 45, more precisely ?? , \[\begin{align} \iint L_M\widetilde{G}_x\,\frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx \le -\lambda_{\mathrm{mic}} \iint \frac{(1+|\xi|)|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx . \end{align}\] For the remaining terms, Young’s inequality and the bilinear collision estimate ?? imply \[\begin{align} &\left| \iint \Bigl(\mathcal{N}(M_x,\widetilde{G})+\mathcal{N}(\widetilde{G},M_x)\Bigr)\frac{\widetilde{G}_x}{M_\#}\,d\xi\,dx \right| \\ &\le \frac{\lambda_{\mathrm{mic}}}{128}\iint \frac{(1+|\xi|)|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx +C\iint \frac{(1+|\xi|)^{-1}}{M_\#} \Bigl( |\mathcal{N}(M_x,\widetilde{G})|^2+|\mathcal{N}(\widetilde{G},M_x)|^2 \Bigr)\,d\xi\,dx . \end{align}\] Now we use the decomposition 43 , namely \[\widetilde{G}=\widetilde{G}_{\text{rem}}+\widetilde{G}_C,\] together with the explicit form of \(\widetilde{G}_C\), the smallness of \((v_x,u_x,\theta_x)\), and the standard bounds for the composite wave. Applying ?? once more, we obtain \[\begin{align} &\iint \frac{(1+|\xi|)^{-1}}{M_\#} \Bigl( |\mathcal{N}(M_x,\widetilde{G})|^2+|\mathcal{N}(\widetilde{G},M_x)|^2 \Bigr)\,d\xi\,dx \\ &\le C(\delta_0+\varepsilon)^2\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 +C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\qquad +C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) +C\frac{\delta_C}{(1+t)^{3/2}} . \end{align}\] Therefore \[\begin{align} \label{eq:GxE-T1} \mathcal{T}_1 &\le -\frac{127}{128}\lambda_{\mathrm{mic}} \int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx \notag\\ &\quad +C(\delta_0+\varepsilon)^2\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 +C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx \notag\\ &\quad +C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) +C\frac{\delta_C}{(1+t)^{3/2}} . \end{align}\tag{149}\]
2. Estimate of \(\mathcal{T}_{2i}\). By Young’s inequality, \[\begin{align} |\mathcal{T}_{2i}| \le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx + C|\dot{X}_i|^2 \int \bigl\lVert\partial_{xx}\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr\rVert_{M_\#}^2\,dx . \end{align}\] By Lemma 4 with \(k=2\), together with translation invariance of the shifted profile, \[\int \bigl\lVert\partial_{xx}\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr\rVert_{M_\#}^2 \,dx \le C\delta_i^7 \le C(\delta_0+\varepsilon)\delta_i .\] Hence \[\label{eq:GxE-T2} |\mathcal{T}_{2i}| \le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)\delta_i|\dot{X}_i|^2 .\tag{150}\]
3. Estimate of \(\mathcal{T}_3\). Expanding the derivative gives \[\begin{align} |\mathcal{T}_3| &\le C\iint \frac{|\widetilde{G}_x||\widetilde{G}_{xx}|}{M_\#}\,d\xi\,dx + C\iint |(u_{1x},v_x)|\frac{|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx . \end{align}\] Using the a priori smallness of \((u_{1x},v_x)\) and Young’s inequality, we obtain \[\label{eq:GxE-T3} |\mathcal{T}_3| \le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx + C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2\,dx .\tag{151}\]
4. Estimate of \(\mathcal{T}_{4i}\). After expanding the \(x\)-derivative and using Young’s inequality, we have \[\begin{align} |\mathcal{T}_{4i}| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C\iint \Bigl| \bigl(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}},\,v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\bigr) \Bigr|^2 \frac{|\partial_{xx}\bigl(G^{S_{i}}\bigr)^{-X_{i}}|^2}{M_\#}\,d\xi\,dx \\ &\quad + C\iint \Bigl| \bigl(u_{1x}-\partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}},\,v_x-\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\bigr) \Bigr|^2 \frac{|\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}|^2}{M_\#}\,d\xi\,dx . \end{align}\] We now use Lemma 4, the shock localization estimate 237 , the interaction lemmas Lemma 7 and Lemma 8, the cutoff estimate Lemma 6, and the previously established macroscopic comparison lemmas Lemma 30–32. This yields \[\begin{align} \label{eq:GxE-T4} |\mathcal{T}_{4i}| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)^2\mathcal{G}_i^S + C\delta_i^3e^{-C\delta_it}\int \eta(U|\overline{U})\,dx \notag\\ &\quad + C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C\delta_i^2\|\phi_x\|_{L^2_x}^2 . \end{align}\tag{152}\]
5. Estimate of \(\mathcal{T}_{5i}\). Using the finite-dimensionality of \(P_1\) and the smooth dependence of the basis \(\{\chi_j\}_{j=0}^4\) on \((v,u,\theta)\), we write \[\bigl(P_1-\bigl(P_1^{S_i}\bigr)\bigr)f = \sum_{j=0}^4 \Bigl[ \langle f,\chi_j\rangle_M\chi_j - \bigl\langle f,\bigl(\chi_j^{S_{i}}\bigr)^{-X_{i}}\bigr\rangle_{S_i}\bigl(\chi_j^{S_{i}}\bigr)^{-X_{i}} \Bigr].\] Hence, after one application of Young’s inequality, \[\begin{align} |\mathcal{T}_{5i}| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\quad + C\int \Biggl[ \int \Bigl\{ \frac{1}{v}P_1(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}) -\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}P_1^{S_i}(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}) \Bigr\}_x \,d\xi \Biggr]^2 dx . \end{align}\] The differentiated coefficient/projector mismatch in the last line is exactly of the same type as the terms treated in Step 5 of the proof of Lemma 35; cf.@eq:eq:kc6-J1 , 145 , and 146 . Using those bounds, together with Lemma 4 for the shock profile moments, we obtain \[\begin{align} \label{eq:GxE-T5} |\mathcal{T}_{5i}| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)^2\mathcal{G}_i^S + C\delta_i^3e^{-C\delta_it}\int \eta(U|\overline{U})\,dx \notag\\ &\quad + C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C\delta_i^2\|\phi_x\|_{L^2_x}^2 . \end{align}\tag{153}\]
6. Estimate of \(\mathcal{T}_6\). This is exactly the differentiated source term treated in Lemma 33. Applying Lemma 33 with \(G=\widetilde{G}_x\) and choosing \(\widetilde{\alpha}>0\) fixed, we get \[\begin{align} \label{eq:GxE-T6} |\mathcal{T}_6| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)^2\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 \notag\\ &\quad + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C\frac{\delta_C}{(1+t)^{3/2}} \notag\\ &\quad + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C\|(\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 \notag\\ &\quad + C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S). \end{align}\tag{154}\]
7. Estimate of \(\mathcal{T}_7\). Using \[(\mathcal{N}(f,g))_x=\mathcal{N}(f_x,g)+\mathcal{N}(f,g_x),\] we have \[(\mathcal{N}(\widetilde{G},\widetilde{G}))_x = \mathcal{N}(\widetilde{G}_x,\widetilde{G})+\mathcal{N}(\widetilde{G},\widetilde{G}_x).\] Therefore, by Young’s inequality and ?? , \[\begin{align} |\mathcal{T}_7| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\quad + C\iint \frac{(1+|\xi|)^{-1}}{M_\#} \Bigl( |\mathcal{N}(\widetilde{G}_x,\widetilde{G})|^2 + |\mathcal{N}(\widetilde{G},\widetilde{G}_x)|^2 \Bigr)\,d\xi\,dx . \end{align}\] Using again 43 , ?? , and the a priori smallness, \[\begin{align} \label{eq:GxE-T7} &|\mathcal{T}_7| \le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\int \bigl\lVert\tilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx\nonumber \\ &\qquad \qquad + C(\delta_0+\varepsilon)^2\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 . \end{align}\tag{155}\]
8. Estimate of \(\mathcal{T}_8\). Expanding the derivative and using ?? , \[\begin{align} |\mathcal{T}_8| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C\sum_{i=1,3}\iint \frac{(1+|\xi|)^{-1}}{M_\#} \Bigl( \bigl|\mathcal{N}\bigl(\widetilde{G}_x,\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\bigr|^2 + \bigl|\mathcal{N}\bigl(\widetilde{G},\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\bigr|^2 \\ & + \bigl|\mathcal{N}\bigl(\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}\bigr)\bigr|^2 + \bigl|\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}_x\bigr)\bigr|^2 \Bigr)\,d\xi\,dx . \end{align}\] By Lemma 4, 43 , the same mixed-collision bookkeeping used in Step 2 of Lemma 35, and in particular 141 , we obtain \[\begin{align} \label{eq:GxE-T8} |\mathcal{T}_8| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx \notag\\ &\quad + C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S) + C(\varepsilon+\delta_0)^2 \bigl(\delta_1^2e^{-C\delta_1t}+\delta_3^2e^{-C\delta_3t}\bigr) \notag\\ &\quad + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int \eta(U|\overline{U})\,dx . \end{align}\tag{156}\]
9. Estimate of \(\mathcal{T}_9\). Similarly, \[\begin{align} |\mathcal{T}_9| & \le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\quad + C\iint \frac{(1+|\xi|)^{-1}}{M_\#} \Bigl( \bigl|\mathcal{N}\bigl(\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(G^{S_{3}}\bigr)^{-X_{3}}\bigr)\bigr|^2 + \bigl|\mathcal{N}\bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}},\partial_x\bigl(G^{S_{3}}\bigr)^{-X_{3}}\bigr)\bigr|^2 \\ & + \bigl|\mathcal{N}\bigl(\partial_x\bigl(G^{S_{3}}\bigr)^{-X_{3}},\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr)\bigr|^2 + \bigl|\mathcal{N}\bigl(\bigl(G^{S_{3}}\bigr)^{-X_{3}},\partial_x\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr)\bigr|^2 \Bigr)\,d\xi\,dx . \end{align}\] By Lemma 4, the exponential localization and separation of the two shifted shock layers, and exactly the same shock–shock interaction estimate as in Step 3 of Lemma 35, cf.@eq:eq:kc6-P3-final , we infer \[\label{eq:GxE-T9} |\mathcal{T}_9| \le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t}.\tag{157}\]
10. Estimate of \(\mathcal{T}_{10}\). Since \[L_M h=\mathcal{N}(M,h)+\mathcal{N}(h,M),\] we have \[\begin{align} &(L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}} \\ &\qquad = \mathcal{N}\bigl(M-\bigl(M^{S_{i}}\bigr)^{-X_{i}},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) +\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},M-\bigl(M^{S_{i}}\bigr)^{-X_{i}}\bigr), \end{align}\] and hence \[\begin{align} & \Bigl((L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}}\Bigr)_x\\ &\qquad = \mathcal{N}\bigl(\bigl(M-\bigl(M^{S_{i}}\bigr)^{-X_{i}}\bigr)_x,\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) +\mathcal{N}\bigl(M-\bigl(M^{S_{i}}\bigr)^{-X_{i}},\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) \\ &\qquad \quad +\mathcal{N}\bigl(\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}},M-\bigl(M^{S_{i}}\bigr)^{-X_{i}}\bigr) +\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},(M-\bigl(M^{S_{i}}\bigr)^{-X_{i}})_x\bigr). \end{align}\] Therefore, by Young’s inequality and ?? , \[\begin{align} |\mathcal{T}_{10}| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C\sum_{i=1,3}\iint \frac{(1+|\xi|)^{-1}}{M_\#} \Bigl( \bigl|\mathcal{N}\bigl((M-\bigl(M^{S_{i}}\bigr)^{-X_{i}})_x,\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\bigr|^2 \\ &\qquad + \bigl|\mathcal{N}\bigl(M-\bigl(M^{S_{i}}\bigr)^{-X_{i}},\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)\bigr|^2 \\ &\qquad + \bigl|\mathcal{N}\bigl(\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}},M-\bigl(M^{S_{i}}\bigr)^{-X_{i}}\bigr)\bigr|^2 \\ &\qquad + \bigl|\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},(M-\bigl(M^{S_{i}}\bigr)^{-X_{i}})_x\bigr)\bigr|^2 \Bigr)\,d\xi\,dx . \end{align}\] Now \((M-\bigl(M^{S_{i}}\bigr)^{-X_{i}})\) and \((M-\bigl(M^{S_{i}}\bigr)^{-X_{i}})_x\) are controlled by \[\begin{align} &\bigl(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}},u-\bigl(u^{S_{i}}\bigr)^{-X_{i}},\theta-\bigl(\theta ^{S_{i}}\bigr)^{-X_{i}}\bigr),\\ &\qquad \bigl(v_x-\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}},u_x-\partial_x\bigl(u^{S_{i}}\bigr)^{-X_{i}},\theta_x-\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\bigr), \end{align}\] respectively. Using Lemma 4, Lemma 6, Lemma 7, Lemma 8, and the macroscopic comparison lemmas Lemma 30–33, we conclude that \[\begin{align} \label{eq:GxE-T10} |\mathcal{T}_{10}| &\le \frac{\lambda_{\mathrm{mic}}}{128}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)^2\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 \notag\\ &\quad + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} \notag\\ &\quad + C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int \eta(U|\overline{U})\,dx . \end{align}\tag{158}\]
Finally, summing 149 , 150 , 151 , 152 , 153 , 154 , 155 , 156 , 157 , and 158 , and absorbing all small fractions of \[\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx\] into the left-hand side, we obtain \[\begin{align} &\frac{d}{dt}\iint \frac{|\widetilde{G}_x|^2}{M_\#}\,d\xi\,dx +\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{M_\#}^2 \,dx \\ &\le C(\delta_0+\varepsilon)^2\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 +C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_Ce^{-Ct}+\delta_3e^{-C\delta_3t}\bigr) +C\frac{\delta_C}{(1+t)^{3/2}} \\ &\quad +C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} +C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} +C\|(\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 \\ &\quad +C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 +C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S) +C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad +C\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \,dx +C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int \eta(U\mid\bar U)\,dx . \end{align}\] This proves the lemma. ◻
Lemma 37. For each \(i=1,3\), one has \[\begin{align} \begin{aligned} & |\ddot X_i|^2 \int \bigl\lVert\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr\rVert_{M_\#}^2 dx \\ & \; \le C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C(\delta_0+\varepsilon)\sum_{j=1,3}\delta_j|\dot{X}_j|^2 \\ &\quad +C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C\frac{\delta_C}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx \\ &\quad + C(\delta_0+\varepsilon) \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#} \,dx + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C(\delta_0+\varepsilon)\delta_0\sum_{i=1,3}\delta_i^2e^{-C\delta_it}. \end{aligned} \label{eq:ddotX-est} \end{align}\qquad{(43)}\]
Proof. By Lemma 4, together with the equivalence between \(M_\#\) and the fixed global Maxwellian near the shock profile, we have \[\label{eq:ddotX-profile} \int_{\mathbb{R}}\bigl\lVert\partial_x \bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr\rVert_{M_\#}^2 \,dx \le C\delta_i^5.\tag{159}\] Hence it suffices to estimate \(\delta_i^3|\ddot X_i|^2\).
Set \[\mathfrak Y_i(t,x) := a(t,x) \Bigl( \partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\,\psi_1 + \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\,\frac{\overline{p}}{\overline{v}}\phi + \frac{\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}}{\overline{\theta}}\zeta \Bigr)(t,x).\] By the definition of the dynamical shifts 40 , \[\dot{X}_i(t) = -\frac{M_i}{\delta_i}\int_{\mathbb{R}}\mathfrak Y_i(t,x)\,dx,\] and therefore \[\ddot X_i(t) = -\frac{M_i}{\delta_i}\int_{\mathbb{R}}\partial_t\mathfrak Y_i(t,x)\,dx .\]
Observe that \[\begin{align} \left| \dot{X}_i\right| \leq C\delta_i^{-1} \bigl\lVert(\phi,\psi_1,\zeta)\bigr\rVert_{L^{\infty}} \int \bigl|\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\bigr| dx \leq C\varepsilon \end{align}\] by the bootstrap assumption. Since \(M_i=O(1)\), it follows that \[\label{eq:ddotX-reduce} \delta_i^3|\ddot X_i|^2 \le C\delta_i\left(\int_{\mathbb{R}}\partial_t\mathfrak Y_i\,dx\right)^2.\tag{160}\]
We decompose \[\partial_t\mathfrak Y_i = a_t\,\mathcal{Z}_i + a\,\partial_t\mathcal{Z}_i, \qquad \mathcal{Z}_i := \partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\,\psi_1 + \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}_x\,\frac{\overline{p}}{\overline{v}}\phi + \frac{\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}}{\overline{\theta}}\zeta.\] Accordingly, write \[\left(\int_{\mathbb{R}}\partial_t\mathfrak Y_i\,dx\right)^2 \le C(I_{i,1}+I_{i,2}+I_{i,3}),\] where \[\begin{align} I_{i,1} &:= \Biggl( \int_{\mathbb{R}} a \Bigl( \partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\,\psi_{1t} + \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\,\frac{\overline{p}}{\overline{v}}\phi_t + \frac{\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}}{\overline{\theta}}\zeta_t \Bigr)\,dx \Biggr)^2,\\ I_{i,2} &:= \left( \int_{\mathbb{R}} a_t\,\mathcal{Z}_i\,dx \right)^2,\\ I_{i,3} &:= \Biggl( \int_{\mathbb{R}} a \Bigl( (\partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}})_t\,\psi_1 + \Bigl(\partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}}\frac{\overline{p}}{\overline{v}}\Bigr)_t\phi + \Bigl(\frac{\partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}}{\overline{\theta}}\Bigr)_t\zeta \Bigr)\,dx \Biggr)^2. \end{align}\]
For \(I_{i,1}\), using Lemma 3, Lemma 5, and the bound \[\int_{\mathbb{R}}|\partial_x(v^{S_i})^{-X_i}|\,dx \le C\delta_i,\] we obtain by Young’s inequality \[\begin{align} I_{i,1} &\le \bigl\lVert\partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}}\bigr\rVert^2_{L_x^2}\, \bigl\lVert(\phi_t,\psi_{1t},\zeta_t)\bigr\rVert_{L^2_x}^2\nonumber\\ &\le C\delta_i^3\|(\phi_t,\psi_{1t},\zeta_t)\|_{L^2_x}^2 . \label{eq:ddotX-I1} \end{align}\tag{161}\]
For \(I_{i,2}\), we differentiate the weight 39 . Since \[a_t = -(\sigma_1+\dot{X}_1)\,\partial_x(a_1)^{-X_1} -(\sigma_3+\dot{X}_3)\,\partial_x(a_3)^{-X_3},\] and \(a_i'=\delta_i^{-1/2}(v^{S_i})'\), Lemma 3 implies \[|a_t| \le C\delta_1^{-1/2}|(v^{S_1})_x^{-X_1}| + C\delta_3^{-1/2}|(v^{S_3})_x^{-X_3}|.\] Therefore, by Young’s inequality, ?? , 237 , Lemma 7, and the exponential separation of the two shocks, \[\begin{align} I_{i,2} &\le C\Bigl(\int \delta_1^{-1/2}|\partial_x \bigl(v^{S_{1}}\bigr)^{-X_{1}}|\,|\partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}}| \,|(\phi,\psi_1,\zeta)| dx \Bigr)^2 \nonumber \\ & \qquad+ C\Bigl(\int \delta_3^{-1/2}|\partial_x \bigl(v^{S_{3}}\bigr)^{-X_{3}}|\,|\partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}}| \,|(\phi,\psi_1,\zeta)| dx \Bigr)^2 \nonumber\\ &\le C\Bigl(\delta_1^{-1}\int |\partial_x \bigl(v^{S_{1}}\bigr)^{-X_{1}}|^2 dx\Bigr)\Bigl(\int |\partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}}|^2\, |(\phi,\psi_1,\zeta)|^2 dx \Bigr) \nonumber \\ &\qquad + C\Bigl(\delta_3^{-1}\int |\partial_x \bigl(v^{S_{3}}\bigr)^{-X_{3}}|^2 dx\Bigr)\Bigl(\int |\partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}}|^2\, |(\phi,\psi_1,\zeta)|^2 dx \Bigr)\nonumber \\ &\le C(\delta_1^2+\delta_3^2) \,\mathcal{G}_i^S + C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\overline{U})\,dx . \label{eq:ddotX-I2} \end{align}\tag{162}\]
For \(I_{i,3}\), we use the shifted-profile identities \[\partial_t \bigl(h^{S_{i}}\bigr)^{-X_{i}} = -(\sigma_i+\dot{X}_i)\partial_x \bigl(h^{S_{i}}\bigr)^{-X_{i}},\] valid for \(h=v^{S_i},u_1^{S_i},\theta^{S_i},G^{S_i}\), together with Lemma 3, Lemma 5, ?? , and ?? . Since each time derivative of a shifted shock profile contributes one additional \(x\)-derivative, we get \[\begin{align} I_{i,3} \le\;& C\delta_i\,\mathcal{G}_i^S + C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\overline{U})\,dx . \label{eq:ddotX-I3} \end{align}\tag{163}\]
Combining 160 , 161 , 162 , and 163 , we arrive at \[\begin{align} \delta_i^3|\ddot X_i|^2 \le & \; C\delta_i\|(\phi_t,\psi_{1t},\zeta_t)\|_{L^2_x}^2 + C\delta_i\mathcal{G}_i^S + C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} \nonumber \\ &\qquad + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\overline{U})\,dx . \label{eq:ddotX-pre} \end{align}\tag{164}\] Now we invoke Lemma 25, namely ?? , and use \(\delta_i\le C(\delta_0+\varepsilon)\). This gives \[\begin{align} \delta_i^3|\ddot X_i|^2 \le\;& C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) \\ &+ C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C(\delta_0+\varepsilon) \int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C\delta_C^2\frac{1}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx + C\frac{\delta_C}{(1+t)^{3/2}} \\ &+ C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\overline{U})\,dx . \end{align}\] Finally, combining this with 159 proves ?? . ◻
Remark 3. This lemma only requires estimating \(\delta_i^5 |\ddot{X}|^2\). However, when estimating the second-order energy, one also needs to estimate 160 . Fortunately, the smallness in the estimate of 160 is still sufficiently good. Indeed, the only term for which the smallness needs to be absorbed is 162 , and even the estimate of 162 can be bounded with more than enough smallness.
Lemma 38. There exists \(C>0\) such that \[\begin{align} \begin{aligned} &\frac{d}{dt}\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{t}\bigr\rVert^2_{M_\#}\,dx + \int_{\mathbb{R}}\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\le C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C\frac{\delta_C}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx \\ &\quad + C(\delta_0+\varepsilon)\delta_0^2\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C\|(\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C\delta_0(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0\sum_{i=1,3}\delta_i^2e^{-C\delta_it} \int_{\mathbb{R}}\eta(U\mid\bar U)\,dx \\ &\quad + C(\delta_0+\varepsilon)\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \,dx + C\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx. \end{aligned} \label{eq:GtE} \end{align}\qquad{(44)}\]
Proof. Differentiating 37 with respect to \(t\), multiplying the resulting equation by \(\widetilde{G}_t/M_\#\), and integrating over \((x,\xi)\in\mathbb{R}\times\mathbb{R}^3\), we obtain
\[\begin{align} \frac{1}{2}\frac{d}{dt}\iint \frac{|\widetilde{G}_t|^2}{M_\#}\,d\xi\,dx = \mathcal{T}_1+\sum_{i=1,3}\mathcal{T}_{2i} +\mathcal{T}_3+\sum_{i=1,3}\mathcal{T}_{4i} +\sum_{i=1,3}\mathcal{T}_{5i} +\mathcal{T}_6+\mathcal{T}_7+\mathcal{T}_8+\mathcal{T}_9+\mathcal{T}_{10}, \end{align}\]
where
\[\begin{align} \mathcal{T}_1 &:= \iint (L_M\widetilde{G})_t\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{2i} &:= \iint \dot{X}_i\,\partial_{xt}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) \frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx + \iint \ddot X_i\,\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_3 &:= \iint \Bigl( \frac{u_1}{v}\widetilde{G}_x-\frac{1}{v}P_1(\xi_1\widetilde{G}_x)\Bigr)_t \frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{4i} &:= \iint \Biggl[ \Bigl( \frac{u_1}{v}-\frac{\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}} \Bigr)\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}} \Biggr]_t \frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{5i} &:= -\iint \Biggl[\frac{1}{v}P_1(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}})-\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}P_1^{S_i}(\xi_1\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}})\Biggr]_t\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_6&:= \iint\Biggl[-\frac{1}{v}P_1(\xi_1M_x)+\frac{1}{\bigl(v^{S_{1}}\bigr)^{-X_{1}}}P_1^{S_1}(\xi_1\partial_x\bigl(M^{S_{1}}\bigr)^{-X_{1}})\Biggr.\\ &\qquad \qquad \Biggl.+\frac{1}{\bigl(v^{S_{3}}\bigr)^{-X_{3}}}P_1^{S_3}(\xi_1\partial_x\bigl(M^{S_{3}}\bigr)^{-X_{3}})\Biggr]_t\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_7&:= \iint \bigl(\mathcal{N}(\widetilde{G},\widetilde{G})\bigr)_t \frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_8&:= \sum_{i=1,3}\iint\Bigl(\mathcal{N}\bigl(\widetilde{G},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)+\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}\bigr)\Bigr)_t\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_9&:= \iint \Bigl[ \mathcal{N}\bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(G^{S_{3}}\bigr)^{-X_{3}}\bigr)+\mathcal{N}\bigl(\bigl(G^{S_{3}}\bigr)^{-X_{3}},\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr) \Bigr]_t \frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx,\\ \mathcal{T}_{10} &:= \sum_{i=1,3}\iint \Bigl( (L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}} \Bigr)_t \frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx. \end{align}\]
Estimate of \(\mathcal{T}_1\). Since \[L_M h=\mathcal{N}(M,h)+\mathcal{N}(h,M),\] we have \[(L_Mh)_t=L_Mh_t+\mathcal{N}(M_t,h)+\mathcal{N}(h,M_t).\] Therefore, \[\begin{align} \mathcal{T}_1 &= \iint L_M\widetilde{G}_t\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx + \iint \Bigl(\mathcal{N}(M_t,\widetilde{G})+\mathcal{N}(\widetilde{G},M_t)\Bigr)\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx. \end{align}\] By the coercivity estimate ?? , \[\iint L_M\widetilde{G}_t\frac{\widetilde{G}_t}{M_\#}\,d\xi\,dx \le -\lambda_{\mathrm{mic}} \iint \frac{(1+|\xi|)|\widetilde{G}_t|^2}{M_\#}\,d\xi\,dx.\] Using Young’s inequality, ?? , the decomposition 43 , and Lemma 25, we obtain \[\begin{align} \label{eq:GtE-T1} \begin{aligned} \mathcal{T}_1 \le\;& -\frac{127}{128}\lambda_{\mathrm{mic}} \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)^2\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C\delta_C^2\frac{1}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx + C\frac{\delta_C}{(1+t)^{3/2}} \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr). \end{aligned} \end{align}\tag{165}\]
Estimate of \(\mathcal{T}_{2i}\). Since \[\partial_t\bigl(G^{S_{i}}\bigr)^{-X_{i}}=-(\sigma_i+\dot{X}_i)\partial_x\bigl(G^{S_{i}}\bigr)^{-X_{i}}, \qquad \partial_{xt}\bigl(G^{S_{i}}\bigr)^{-X_{i}}=-(\sigma_i+\dot{X}_i)\partial_{xx}\bigl(G^{S_{i}}\bigr)^{-X_{i}},\] Lemma 4 yields \[\iint \frac{|\bigl((G^{S_{i}})^{-X_{i}}\bigr)_{xt}|^2}{M_\#}\,d\xi\,dx \le C\delta_i^7 \le C(\delta_0+\varepsilon)\delta_i .\] Therefore, by Young’s inequality and Lemma 37, \[\begin{align} \label{eq:GtE-T2} \begin{aligned} |\mathcal{T}_{2i}| \le\;& \frac{\lambda_{\mathrm{mic}}}{64} \int \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\delta_i|\dot{X}_i|^2 \\ &+ C(\delta_0+\varepsilon)^2\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S) \\ &+ C(\delta_0+\varepsilon)\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C\delta_C^2\frac{1}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx + C\frac{\delta_C}{(1+t)^{3/2}} \\ &+ C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{aligned} \end{align}\tag{166}\]
Estimate of \(\mathcal{T}_3\). Expanding the time derivative gives terms of the form \[\frac{u_{1t}}{v}\widetilde{G}_x,\qquad \frac{u_1}{v}\widetilde{G}_{xt},\qquad \frac{v_t}{v^2}P_1(\xi_1\widetilde{G}_x),\qquad \frac{1}{v}(P_1)_t(\xi_1\widetilde{G}_x),\qquad \frac{1}{v}P_1(\xi_1\widetilde{G}_{xt}).\] Using Young’s inequality, the boundedness of \(P_1\), and Lemma 25, we get \[\begin{align} \label{eq:GtE-T3} \begin{aligned} |\mathcal{T}_3| \le\;& \frac{\lambda_{\mathrm{mic}}}{128} \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx + C\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)^2\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C\delta_C^2\frac{1}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx . \end{aligned} \end{align}\tag{167}\]
Estimate of \(\mathcal{T}_{4i}\), \(\mathcal{T}_{5i}\), \(\mathcal{T}_6\), and \(\mathcal{T}_{10}\). These are the time-differentiated counterparts of the corresponding terms in the proof of Lemma 36. When the derivative falls on a macroscopic coefficient, we use Lemma 25; when it falls on the projected polynomial moments, we use Lemmas 33–35; and when it falls on a shifted shock profile, we use the identities \[\partial_t \bigl(h^{S_{i}}\bigr)^{-X_{i}} = -(\sigma_i+\dot{X}_i)\partial_x \bigl(h^{S_{i}}\bigr)^{-X_{i}}, \qquad h=v^{S_i},u_1^{S_i},\theta^{S_i},G^{S_i},\] together with Lemmas 3–5, Lemma 6, Lemma 7, and Lemma 8. Proceeding exactly as in Lemma 36, we obtain \[\begin{align} \label{eq:GtE-T45610} \begin{aligned} &\sum_{i=1,3}\bigl(|\mathcal{T}_{4i}|+|\mathcal{T}_{5i}|\bigr)+|\mathcal{T}_6|+|\mathcal{T}_{10}| \\ &\le \frac{\lambda_{\mathrm{mic}}}{16} \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)^2\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &\quad + C\|(\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S) + C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 \\ &\quad + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C\delta_C^2\frac{1}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx + C\frac{\delta_C}{(1+t)^{3/2}} \\ &\quad + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} \\ &\quad + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid \bar U)\,dx . \end{aligned} \end{align}\tag{168}\]
Estimate of \(\mathcal{T}_7\), \(\mathcal{T}_8\), and \(\mathcal{T}_9\). Using \[(\mathcal{N}(f,g))_t=\mathcal{N}(f_t,g)+\mathcal{N}(f,g_t),\] together with ?? , Lemma 4, and the same bookkeeping as in 141 –142 , we infer \[\begin{align} \begin{aligned} |\mathcal{T}_7|+|\mathcal{T}_8| \le\;& \frac{\lambda_{\mathrm{mic}}}{64} \iint \frac{(1+|\xi|)|\widetilde{G}_t|^2}{M_\#}\,d\xi\,dx \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C(\delta_0+\varepsilon)^2(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &+ C(\varepsilon+\delta_0)^2\bigl(\delta_1^2e^{-C\delta_1t}+\delta_3^2e^{-C\delta_3t}\bigr) + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx , \end{aligned} \end{align}\] and \[\label{eq:GtE-T9} |\mathcal{T}_9| \le \frac{\lambda_{\mathrm{mic}}}{128} \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t}.\tag{169}\]
Finally, summing 165 , 166 , 167 , 168 , and 169 , and absorbing all small fractions of \[\int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx\] into the left-hand side, we obtain ?? . This completes the proof. ◻
For later use, set \[\mathcal{M} := M-\bigl(M^{S_{1}}\bigr)^{-X_{1}}-\bigl(M^{S_{3}}\bigr)^{-X_{3}}, \qquad \widetilde{f} = \widetilde{G}+\mathcal{M} .\] We repeatedly use the standard Maxwellian expansion estimate \[\begin{align} \label{eq:f-high-macro-part} &\bigl\lVert\partial^{\alpha_0}_t\partial^{\alpha_1}_x\mathcal{M}\bigr\rVert_{M_\#}^2 \le C\Big( \varphi_1^2\bigl|\partial_t^{\alpha_0}\partial_x^{\alpha_1}\bigl(U-\bigl(U^{S_{1}}\bigr)^{-X_{1}}\bigr)\bigr|^2 +\varphi_1^2\bigl|\partial_t^{\alpha_0}\partial_x^{\alpha_1} \bigl(U^{S_{3}}\bigr)^{-X_{3}}\bigr|^2 \nonumber \\ &\qquad +\varphi_3^2\bigl|\partial_t^{\alpha_0}\partial_x^{\alpha_1}\bigl(U-\bigl(U^{S_{3}}\bigr)^{-X_{3}}\bigr)\bigr|^2 +\varphi_3^2\bigl|\partial_t^{\alpha_0}\partial_x^{\alpha_1} \bigl(U^{S_{1}}\bigr)^{-X_{1}}\bigr|^2 \Big), \end{align}\tag{170}\] for \(|\alpha_0|+|\alpha_1|\le 2\), where \(U=(v,u,\theta)\) and \(\bigl(U^{S_{i}}\bigr)^{-X_{i}}=\bigl(\bigl(v^{S_{i}}\bigr)^{-X_{i}},\bigl(u^{S_{i}}\bigr)^{-X_{i}},\bigl(\theta^{S_{i}}\bigr)^{-X_{i}}\bigr)\).
Lemma 39. There exists a constant \(C>0\) such that \[\begin{align} \begin{aligned} &\frac{d}{dt}\iint_{\mathbb{R}}\bigl\lVert\widetilde{f}_{xx}\bigr\rVert^2_{M_\#} \,dx +\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\le C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C(\delta_0+\varepsilon)\delta_0^2\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &\quad + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C\delta_0\sum_{i=1,3}\delta_i^2e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C\frac{\delta_C}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx . \end{aligned} \label{eq:ftxE} \end{align}\qquad{(45)}\]
Proof. We start from the perturbed equation for \(\widetilde{f}\): \[\begin{align} \begin{aligned} &v\widetilde{f}_t-u_1\widetilde{f}_x+\xi_1\widetilde{f}_x -\sum_{i=1,3}v\dot{X}_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}} +\sum_{i=1,3} v\Bigl( \frac{\xi_1-u_1}{v}-\frac{\xi_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}} \Bigr)\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}} \\ &= vL_M\widetilde{G} + v\mathcal{N}(\widetilde{G},\widetilde{G}) + v\sum_{i=1,3}\Bigl((L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}}\Bigr) \\ &\quad + v\sum_{i=1,3} \Bigl( \mathcal{N}\bigl(\widetilde{G},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr) + \mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}\bigr) \Bigr) \\ &\quad+ v\Bigl( \mathcal{N}\bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(G^{S_{3}}\bigr)^{-X_{3}}\bigr) + \mathcal{N}\bigl(\bigl(G^{S_{3}}\bigr)^{-X_{3}},\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr) \Bigr). \end{aligned} \label{eq:ftx-start} \end{align}\tag{171}\] Apply \(\partial_t\partial_x\) to 171 , multiply by \(\widetilde{f}_{tx}/M_\#\), and integrate over \((x,\xi)\in\mathbb{R}\times\mathbb{R}^3\). We write the resulting terms as \[\mathcal{I}_1+\mathcal{I}_2+\sum_{i=1,3}\mathcal{I}_{3i} +\sum_{i=1,3}\mathcal{I}_{4i} +\mathcal{I}_5+\sum_{i=1,3}\mathcal{I}_{6i} +\sum_{i=1,3}\mathcal{I}_{7i} +\mathcal{I}_8+\mathcal{I}_9,\] corresponding respectively to \[(v\widetilde{f}_t)_{tx},\quad (u_1\widetilde{f}_x)_{tx},\quad \Bigl(v\dot{X}_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}}\Bigr)_{tx},\quad \Biggl( v\Bigl(\frac{\xi_1-u_1}{v}-\frac{\xi_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\Bigr)\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}} \Biggr)_{tx},\] \[(v\mathcal{N}(\widetilde{G},\widetilde{G}))_{tx},\quad \bigl(v(L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)_{tx},\quad \Bigl( v\bigl(\mathcal{N}\bigl(\widetilde{G},\bigl(G^{S_{i}}\bigr)^{-X_{i}}\bigr)+\mathcal{N}\bigl(\bigl(G^{S_{i}}\bigr)^{-X_{i}},\widetilde{G}\bigr)\bigr) \Bigr)_{tx},\] \[(vL_M\widetilde{G})_{tx},\qquad \Bigl( v\bigl(\mathcal{N}\bigl(\bigl(G^{S_{1}}\bigr)^{-X_{1}},\bigl(G^{S_{3}}\bigr)^{-X_{3}}\bigr)+\mathcal{N}\bigl(\bigl(G^{S_{3}}\bigr)^{-X_{3}},\bigl(G^{S_{1}}\bigr)^{-X_{1}}\bigr)\bigr) \Bigr)_{tx}.\]
Step 1: the transport terms \(\mathcal{I}_1+\mathcal{I}_2\). Expanding derivatives, we have \[\begin{align} \mathcal{I}_1 &= \iint \frac{(v\widetilde{f}_t)_{tx}\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx \\ &= \iint \frac{v_{tx}\widetilde{f}_t\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx + \iint \frac{(v_t\widetilde{f}_{xx}+v_x\widetilde{f}_{tt})\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx + \iint \frac{v\widetilde{f}_{ttx}\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx. \end{align}\] The last term gives \[\iint \frac{v\widetilde{f}_{ttx}\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx = \frac{d}{dt}\iint \frac{v|\widetilde{f}_{tx}|^2}{2M_\#}\,d\xi\,dx - \iint \frac{v_t|\widetilde{f}_{tx}|^2}{2M_\#}\,d\xi\,dx.\] Since \(v\) is uniformly comparable to a positive constant, the energy \(\iint v|\widetilde{f}_{tx}|^2/M_\#\) is equivalent to \(\iint |\widetilde{f}_{tx}|^2/M_\#\). Next, using \[\widetilde{f}_{tx}=\widetilde{G}_{tx}+\mathcal{M}_{tx}, \qquad \widetilde{f}_t=\widetilde{G}_t+\mathcal{M}_t,\] together with 170 , Lemma 25, and Young’s inequality, we get \[\begin{align} \begin{aligned} |\mathcal{I}_1| \le\;& \frac{d}{dt}\iint \frac{v|\widetilde{f}_{tx}|^2}{2M_\#}\,d\xi\,dx + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &+ C\frac{\delta_C}{(1+t)^{3/2}} + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} \\ &+ C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\overline{U})\,dx + C\delta_C^2\frac{1}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx . \end{aligned} \label{eq:ftx-I1} \end{align}\tag{172}\]
Similarly, \[\mathcal{I}_2 = -\iint \frac{(u_1\widetilde{f}_x)_{tx}\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx .\] Expanding derivatives and integrating by parts in \(x\) in the top-order term \(\iint u_1\widetilde{f}_{txx}\widetilde{f}_{tx}/M_\#\), we obtain \[\begin{align} \begin{aligned} |\mathcal{I}_2| \le\;& C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 +\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &+ C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{aligned} \label{eq:ftx-I2} \end{align}\tag{173}\]
Step 2: the shift term \(\mathcal{I}_{3i}\). Since \[\partial_t\bigl(F^{S_{i}}\bigr)^{-X_{i}} = -(\sigma_i+\dot{X}_i)\partial_x \bigl(F^{S_{i}}\bigr)^{-X_{i}}, \qquad \partial_{tx}\bigl(F^{S_{i}}\bigr)^{-X_{i}} = -(\sigma_i+\dot{X}_i)\partial_{xx}\bigl(F^{S_{i}}\bigr)^{-X_{i}},\] we may expand \[\begin{align} (v\dot{X}_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}})_{tx} &= v_{tx}\dot{X}_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}} + v_t\dot{X}_i\partial_{xx}\bigl(F^{S_{i}}\bigr)^{-X_{i}} + v_x\ddot X_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}} \\ &\quad + v_x\dot{X}_i\partial_{tx}\bigl(F^{S_{i}}\bigr)^{-X_{i}} + v\ddot X_i\partial_{xx}\bigl(F^{S_{i}}\bigr)^{-X_{i}} + v\dot{X}_i\partial_{txx}\bigl(F^{S_{i}}\bigr)^{-X_{i}}\\ &=:\sum_{l=1}^5 \mathcal{I}_{3i}^l \end{align}\]
For each term, we have the following estimates.
\[\begin{align} &|\mathcal{I}_{3i}^1| \le C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{f}_{tx}\bigr\rVert_{M_\#}^2 dx +C(\delta_0+\varepsilon)\delta_i|\dot{X}_i|^2 \\ &|\mathcal{I}_{3i}^3| + |\mathcal{I}_{3i}^5| \le C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{f}_{tx}\bigr\rVert_{M_\#}^2 dx + C\delta_i^3 |\ddot{X}_i|^2\\ &|\mathcal{I}_{3i}^2|+|\mathcal{I}_{3i}^4| +|\mathcal{I}_{3i}^6| \le C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{f}_{tx}\bigr\rVert_{M_\#}^2 dx + C(\delta_0+\varepsilon)\delta_i|\dot{X}_i|^2 \end{align}\]
By Young’s inequality, 164 , 173 , Lemma 4, and Lemma 37, we obtain \[\begin{align} \begin{aligned} |\mathcal{I}_{3i}| \le\;& C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\delta_i|\dot{X}_i|^2 \\ &+ C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C\frac{\delta_C}{(1+t)^{3/2}} + C\delta_C^2\frac{1}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx \\ &+ C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{aligned} \label{eq:ftx-I3} \end{align}\tag{174}\]
Step 3: the coefficient-mismatch term \(\mathcal{I}_{4i}\). Write \[\begin{align} &\frac{\xi_1-u_1}{v}-\frac{\xi_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}\\ &\quad = -\frac{\xi_1}{v\bigl(v^{S_{i}}\bigr)^{-X_{i}}}(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}) +\frac{u_1}{v\bigl(v^{S_{i}}\bigr)^{-X_{i}}}(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}) -\frac{1}{\bigl(v^{S_{i}}\bigr)^{-X_{i}}}(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}). \end{align}\] After applying \(\partial_{tx}\), every term is a linear combination of products of:
a first- or second-order macroscopic derivative of \(v,u_1\),
a factor \(v-\bigl(v^{S_{i}}\bigr)^{-X_{i}}\) or \(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\),
and a profile derivative \(\partial_t^{\gamma_0}\partial_x^{\gamma_1} \bigl(F^{S_{i}}\bigr)^{-X_{i}}\) with \(|\gamma|=|\gamma_0|+|\gamma_1|\le 3\).
Therefore, using Young’s inequality, Lemma 4, Lemma 6, Lemma 7, Lemma 8, and the same weighted shock-interaction bounds as in Lemma 36, we get \[\begin{align} \begin{aligned} |\mathcal{I}_{4i}| \le\;& C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\mathcal{G}_i^S \\ &+ C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &+ C(\varepsilon+\delta_0)^2\delta_i^2e^{-C\delta_it} + C\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{aligned} \label{eq:ftx-I4} \end{align}\tag{175}\]
Step 4: the quadratic nonlinear term \(\mathcal{I}_5\). Expanding by Leibniz’ rule, \[(v\mathcal{N}(\widetilde{G},\widetilde{G}))_{tx} = v_{tx}\mathcal{N}(\widetilde{G},\widetilde{G}) + v_t\bigl(\mathcal{N}(\widetilde{G}_x,\widetilde{G})+\mathcal{N}(\widetilde{G},\widetilde{G}_x)\bigr)\] \[\qquad + v_x\bigl(\mathcal{N}(\widetilde{G}_t,\widetilde{G})+\mathcal{N}(\widetilde{G},\widetilde{G}_t)\bigr) + v\bigl(\mathcal{N}(\widetilde{G}_{tx},\widetilde{G})+\mathcal{N}(\widetilde{G}_t,\widetilde{G}_x) +\mathcal{N}(\widetilde{G}_x,\widetilde{G}_t)+\mathcal{N}(\widetilde{G},\widetilde{G}_{tx})\bigr).\] Using ?? , the one-dimensional Sobolev bound \[\left\| \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \right\|_{L^\infty_x} \le C\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2\,dx,\] and Young’s inequality, we infer \[\begin{align} \begin{aligned} |\mathcal{I}_5| \le\;& C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &+ C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &+ C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{aligned} \label{eq:ftx-I5} \end{align}\tag{176}\]
Step 5: the mixed shock terms \(\mathcal{I}_{6i}\), \(\mathcal{I}_{7i}\), and \(\mathcal{I}_9\). These terms are handled exactly as above by combining:
the bilinear collision estimate ?? ,
the profile bounds from Lemma 4,
and the already established lower-order bounds in Lemma 36 and Lemma 38.
In particular, differentiating \[(L_M-L_{i}^S)\bigl(G^{S_{i}}\bigr)^{-X_{i}}\] in \((t,x)\) produces only coefficient mismatches of first and second order, hence these terms are of the same type as in Step 4 and the proof of Lemma 36. Consequently, \[\begin{align} \begin{aligned} &\sum_{i=1,3}\bigl(|\mathcal{I}_{6i}|+|\mathcal{I}_{7i}|\bigr)+|\mathcal{I}_9| \\ &\le C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2\,dx + C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) \\ &\quad + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^ + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) + C\frac{\delta_C}{(1+t)^{3/2}} \\ &\quad + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{aligned} \label{eq:ftx-I679} \end{align}\tag{177}\]
Step 6: the linear collision term \(\mathcal{I}_8\). This is where the coercive term appears. By differentiating \(vL_M\widetilde{G}\), we write \[(vL_M\widetilde{G})_{tx} = vL_M\widetilde{G}_{tx} +\mathcal{R}_{tx},\] where \(\mathcal{R}_{tx}\) is a sum of lower-order terms involving \(v_t,v_x,v_{tx}\), \(M_t,M_x,M_{tx}\), and \(\widetilde{G},\widetilde{G}_t,\widetilde{G}_x\). Hence \[\mathcal{I}_8 = \iint \frac{vL_M\widetilde{G}_{tx}\,\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx + \iint \frac{\mathcal{R}_{tx}\,\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx .\] Using \(\widetilde{f}_{tx}=\widetilde{G}_{tx}+\mathcal{M}_{tx}\), we split the first term: \[\begin{align} \iint \frac{vL_M\widetilde{G}_{tx}\,\widetilde{f}_{tx}}{M_\#}\,d\xi\,dx = \iint \frac{v\widetilde{G}_{tx}L_M\widetilde{G}_{tx}}{M_\#}\,d\xi\,dx + \iint \frac{vL_M\widetilde{G}_{tx}\,\mathcal{M}_{tx}}{M_\#}\,d\xi\,dx . \end{align}\] By ?? , \[\iint \frac{v\widetilde{G}_{tx}L_M\widetilde{G}_{tx}}{M_\#}\,d\xi\,dx \le -\lambda_{\mathrm{mic}} \int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx .\] The cross term with \(\mathcal{M}_{tx}\) is controlled by 170 , Lemma 25, and Young’s inequality; the remainder \(\mathcal{R}_{tx}\) is estimated by ?? exactly as in Steps 1, 4, and 5. Thus \[\begin{align} \begin{aligned} \mathcal{I}_8 \le\;& -\frac{127}{128}\lambda_{\mathrm{mic}} \int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &+ C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 +\bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx \\ &+ C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^3\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &+ C\frac{\delta_C}{(1+t)^{3/2}} + C(\varepsilon+\delta_0)^2\delta_1^2e^{-C\delta_1t} + C(\varepsilon+\delta_0)^2\delta_3^2e^{-C\delta_3t} \\ &+ C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx + C\delta_C^2\frac{1}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx . \end{aligned} \label{eq:ftx-I8} \end{align}\tag{178}\]
Finally, summing 172 , 173 , 174 , 175 , 176 , 177 , and 178 , and absorbing the small multiples of \[\int \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2 \,dx\] into the left-hand side, we obtain ?? . ◻
Lemma 40. There exists a constant \(C>0\) such that \[\begin{align} \begin{aligned} &\frac{d}{dt}\int_{\mathbb{R}}\bigl\lVert\widetilde{f}_{xx}\bigr\rVert^2_{M_\#}\,dx +\int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu, M_\#}^2 \,dx \\ &\le C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^2(\delta_0+\varepsilon)\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &\quad + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C\delta_0\sum_{i=1,3}\delta_i^2e^{-C\delta_it}\int_{\mathbb{R}}\eta(U|\overline{U})\,dx+ C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 +\bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2\,dx + C\frac{\delta_C}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx . \end{aligned} \label{eq:fxxE} \end{align}\qquad{(46)}\]
Proof sketch. Apply \(\partial_x^2\) to 171 , multiply by \(\widetilde{f}_{xx}/M_\#\), and integrate over \((x,\xi)\in\mathbb{R}\times\mathbb{R}^3\). The resulting terms are treated by the same decomposition as in the proof of Lemma 39, with the following simplifications.
(1) There is no \(\ddot X_i\)-term. Indeed, \[\partial_x^2(v\dot{X}_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}}) = v_{xx}\dot{X}_i\partial_x\bigl(F^{S_{i}}\bigr)^{-X_{i}} + 2v_x\dot{X}_i\partial_{xx}\bigl(F^{S_{i}}\bigr)^{-X_{i}} + v\dot{X}_i\partial^3_x\bigl(F^{S_{i}}\bigr)^{-X_{i}},\] so only \(\dot{X}_i\) appears. Hence the shift contribution is easier than in the \(\widetilde{f}_{tx}\)-estimate and is controlled directly by Lemma 4 and Young’s inequality.
(2) The coercive term again comes from \((vL_M\widetilde{G})_{xx}\). Writing \[(vL_M\widetilde{G})_{xx}=vL_M\widetilde{G}_{xx}+\mathcal{R}_{xx},\] we have \[\iint \frac{vL_M\widetilde{G}_{xx}\,\widetilde{f}_{xx}}{M_\#}\,d\xi\,dx = \iint \frac{v\widetilde{G}_{xx}L_M\widetilde{G}_{xx}}{M_\#}\,d\xi\,dx + \iint \frac{vL_M\widetilde{G}_{xx}\,\mathcal{M}_{xx}}{M_\#}\,d\xi\,dx .\] The first term is estimated by ?? ; the second by 170 , exactly as in Step 6 of Lemma 39.
(3) The only terms which are genuinely different from the \(\widetilde{f}_{tx}\)-case are those where two spatial derivatives hit the transport coefficients. A representative example is \[\iint \frac{v_{xx}\widetilde{f}_t\,\widetilde{f}_{xx}}{M_\#}\,d\xi\,dx .\] Using \(\widetilde{f}_t=\widetilde{G}_t+\mathcal{M}_t\), Young’s inequality, 170 , and Lemma 25, we obtain \[\begin{align} & \left| \iint \frac{v_{xx}\widetilde{f}_t\,\widetilde{f}_{xx}}{M_\#}\,d\xi\,dx \right| \\ &\quad \le C(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 \\ &\qquad + C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 + C\delta_C^2\frac{1}{1+t}\int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx \\ &\qquad + C\frac{\delta_C}{(1+t)^{3/2}} + C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\sum_{i=1,3}\delta_i^3e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx . \end{align}\] The term with \(u_{1xx}\widetilde{f}_x\widetilde{f}_{xx}\) is handled in the same way.
(4) All remaining terms are identical in structure to those treated in the proof of Lemma 39, with \(t\)-derivatives replaced by \(x\)-derivatives. Hence they are estimated by the same ingredients: Lemma 4, Lemma 6, Lemma 7, Lemma 8, Lemma 36, Lemma 38, Lemma 25, and ?? .
Collecting all contributions and absorbing the small multiples of \[\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \,dx\] into the left-hand side, we obtain ?? . ◻
Corollary 2. There exists a constant \(C>0\) such that \[\begin{align} \begin{aligned} &\frac{d}{dt}\int_{\mathbb{R}}\bigl\lVert\widetilde{f}_{xx}\bigr\rVert^2_{M_\#}+\bigl\lVert\widetilde{f}_{tx}\bigr\rVert^2_{M_\#}\,dx + \int_{\mathbb{R}}\bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{\nu,M_\#}^2\,dx \\ &\le C(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C(\delta_0+\varepsilon)(\mathcal{G}_1^S+\mathcal{G}_3^S) + C\delta_0^2(\delta_0+\varepsilon)\bigl(\delta_1e^{-C\delta_1t}+\delta_3e^{-C\delta_3t}\bigr) \\ &\quad + C\frac{\delta_C}{(1+t)^{\frac{5}{4}}} + C\delta_0\sum_{i=1,3}\delta_i^2e^{-C\delta_it}\int_{\mathbb{R}}\eta(U\mid\bar U)\,dx+ C(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\|(\phi_{xx},\psi_{xx},\zeta_{xx})\|_{L^2_x}^2 + C(\delta_0+\varepsilon)\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 \\ &\quad + C(\delta_0+\varepsilon)\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_{xt}\bigr\rVert_{\nu,M_\#}^2\,dx + C\frac{\delta_C}{1+t} \int_{\mathbb{R}}e^{-\frac{2c_0|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx . \end{aligned} \end{align}\]
Proof. This follows immediately by adding ?? and ?? . ◻
We define a Gaussian-weighted spacetime functional: \[\begin{align} \label{def:W} \mathcal{W}_C(T) := \int_0^T \frac{1}{1+t}\int_{\mathbb{R}} e^{-\frac{2c|x|^2}{1+t}} |(\phi,\psi,\zeta)|^2\,dx\,dt, \end{align}\tag{179}\] and \[\begin{align} \label{eq:kinetic-high-good} \mathcal{K}_{\mathrm{high}}(t):= \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_{xt}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2\,dx \end{align}\tag{180}\]
Proposition 7. Under the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 , there exists a constant \(C>0\) such that \[\begin{align} \begin{aligned} &\sup_{t\in[0,T]} \left\{ \|(\phi_x,\psi_x,\zeta_x)(t)\|_{L^2_x}^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{f}_{xx}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{f}_{xt}\bigr\rVert_{M_\#}^2\,dx \right\} \\ &\quad + \int_0^T \|(\phi_{xx},\psi_{xx},\zeta_{xx},\phi_{xt},\psi_{xt},\zeta_{xt})(t)\|_{L^2_x}^2\,dt + \int_0^T \mathcal{K}_{\mathrm{high}}(t) \,dt \\ &\le C \mathcal{E}(0)^2 + C\delta_0^{\frac{1}{2}} + C(\delta_0+\varepsilon) \int_0^T \sum_{i=1,3}\delta_i |\dot{X}_i|^2\,dt + C(\delta_0+\varepsilon)\int_0^T \sum_{i=1,3}\mathcal{G}_i^S\,dt \\ &\quad + C(\delta_0+\varepsilon) \int_0^T \sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2\,dt + C(\delta_0+\varepsilon)\int_0^T \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx\,dt \\ &\quad + C\delta_C\mathcal{W}_C(T). \end{aligned} \label{eq:high-order-closure} \end{align}\qquad{(47)}\]
Proof. We combine the previously established high-order differential estimates: the second-order macroscopic estimate, Lemma 36, Lemma 38, Lemma 39, and Lemma 40. Thus there exist positive constants \(C_1,\dots,C_5\) such that, for any positive parameters \(\lambda_1,\lambda_2,\lambda_3,\lambda_4\), one has \[\begin{align} \begin{aligned} &\frac{d}{dt} \Bigg\{ \|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 +\lambda_1\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{M_\#}^2 \,dx +\lambda_2\int_{\mathbb{R}} \bigl\lVert\widetilde{f}_{xx}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{f}_{xt}\bigr\rVert_{M_\#}^2\,dx \Bigg\} \\ &\quad +\int_{\mathbb{R}} \bigl( \lambda_4 \phi_{xx}^2+\psi_{1xx}^2+\psi_{2xx}^2+\psi_{3xx}^2+\zeta_{xx}^2 \bigr)\,dx +\lambda_3\|(\phi_{xt},\psi_{xt},\zeta_{xt})\|_{L^2_x}^2 \\ &\quad +\frac{\lambda_1}{2}\int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 \,dx +\frac{\lambda_2}{2}\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xt}\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\le C_{\mathrm{high}}(\delta_0+\varepsilon)\sum_{i=1,3}\delta_i|\dot{X}_i|^2 + C_{\mathrm{high}}(\delta_0+\varepsilon)\sum_{i=1,3}\mathcal{G}_i^S + C_{\mathrm{high}}(\delta_0+\varepsilon)\sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2 \\ &\quad + C_{\mathrm{high}}(\delta_0+\varepsilon)\int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx + C_{\mathrm{high}}\delta_C^2 \frac{1}{1+t}\int_{\mathbb{R}}e^{-\frac{2c|x|^2}{1+t}}|(\phi,\psi,\zeta)|^2\,dx \\ &\quad + C_{\mathrm{mic}1}\int \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 \,dx + C_{\mathrm{mic}2}\int \bigl\lVert\widetilde{G}_{xt}\bigr\rVert_{\nu,M_\#}^2 \,dx \\ &\quad + C_{\mathrm{mic}3}\int \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{\nu,M_\#}^2 \,dx + C_{\mathrm{mic}4}\int \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{\nu,M_\#}^2 \,dx + \lambda_4\frac{d}{dt}\int_{\mathbb{R}}\phi_{xx}\psi_{1x}\,dx , \end{aligned} \label{eq:high-order-precombine} \end{align}\tag{181}\] where \[C_{\mathrm{high}}:=C_1+\lambda_1C_2+\lambda_2C_3+\lambda_3C_4+\lambda_4C_5,\] and similarly \(C_{\mathrm{mic}1},C_{\mathrm{mic}2},C_{\mathrm{mic}3},C_{\mathrm{mic}4}\) denote the corresponding linear combinations of \(C_1,\dots,C_5\).
Choose \(\lambda_1,\lambda_2,\lambda_3,\lambda_4\) successively so that \[\begin{align} C_{\mathrm{mic}1}<\frac{\lambda_2}{4}, \qquad C_{\mathrm{mic}2}<\frac{\lambda_2}{4}, \qquad C_{\mathrm{mic}3}<\frac{\lambda_1}{8}, \qquad C_{\mathrm{mic}4}<\frac{\lambda_1}{8}. \label{eq:gamma-choice-1} \end{align}\tag{182}\] Then the four kinetic terms on the right-hand side of 181 are absorbed into the left-hand side.
Next, move the derivative term to the left and define \[\begin{align} &\mathcal{E}_h(t) := \|(\phi_x,\psi_x,\zeta_x)(t)\|_{L^2_x}^2 +\lambda_1\int \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{G}_{t}\bigr\rVert_{M_\#}^2 \,dx \nonumber\\ &\quad +\lambda_2\int \bigl\lVert\widetilde{f}_{xx}\bigr\rVert_{M_\#}^2 + \bigl\lVert\widetilde{f}_{xt}\bigr\rVert_{M_\#}^2 \,dx -\lambda_4\int_{\mathbb{R}}\phi_{xx}\psi_{1x}\,dx . \label{eq:high-order-modified-energy} \end{align}\tag{183}\]
By Young’s inequality, for any \(\kappa_1>0\), \[\begin{align} \begin{aligned} \lambda_4\left|\int_{\mathbb{R}}\phi_{xx}\psi_{1x}\,dx\right| \le& \kappa_1\|\phi_{xx}\|_{L^2_x}^2 + C_{\kappa_1}\lambda_4^2\|\psi_{1x}\|_{L^2_x}^2 \\ \le&\kappa_1\iint \frac{\left| \widetilde{f}_{xx}\right|^2}{M_\#} d\xi dx + C\kappa_1\varepsilon^2\bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 + C\kappa_1\delta + C_{\kappa_1} \lambda_4^2 \bigl\lVert\psi_{1x}\bigr\rVert_{L^2}^2. \end{aligned} \label{eq:young-cross-high} \end{align}\tag{184}\] Choose \(\kappa_1>0\) sufficiently small so that the first term on the right-hand side of 184 is absorbed into the \(\lambda_4\phi_{xx}^2\)-term already present on the left-hand side of 181 . Since \(\psi_{1x}\) is lower order, the second term is controlled by the low-order energy. Hence, for \(\lambda_4\) sufficiently small, the modified energy \(\mathcal{E}_h(t)\) is equivalent to \[\|(\phi_x,\psi_x,\zeta_x)(t)\|_{L^2_x}^2 + \mathcal{K}_{\mathrm{high}}\] up to a harmless multiple of \(\|(\phi_x,\psi_x,\zeta_x)(t)\|_{L^2_x}^2\).
Integrating in time over \([0,T]\), using 182 , and absorbing the cross term contribution yields ?? . ◻
We here complete the proof of the main a priori estimate stated in Proposition 1. The zeroth-order analysis of Section 5 already controls the basic \(L^2_x\)-size of the perturbation, the shock coercive terms \(\mathcal{G}_i^S\), the modulation terms \(\delta_i|\dot{X}_i|^2\), and the zeroth-order microscopic dissipation. The differentiated analysis of Section 6 then supplies the remaining first- and second-order macroscopic bounds together with the differentiated microscopic estimates. Thus, at this stage, the only quantity not yet directly absorbed into the main a priori norm is the Gaussian-weighted space–time term \(\mathcal{W}_C(T)\) of 179 : \[\mathcal{W}_C(T) := \int_0^T \frac{1}{1+t}\int_{\mathbb{R}} e^{-\frac{2c|x|^2}{1+t}} |(\phi,\psi,\zeta)(t,x)|^2\,dx\,dt .\] The following lemma shows that \(\mathcal{W}_C(T)\) is itself controlled by the quantities already appearing in the zeroth- and differentiated estimates.
Lemma 41. Under the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 , there exists a constant \(C>0\) such that \[\begin{align} \mathcal{W}_C(T) \le\;& C\sup_{t\in[0,T]}\|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 + C\int_0^T \sum_{i=1,3}\delta_i |\dot{X}_i|^2\,dt + C\int_0^T \sum_{i=1,3}\mathcal{G}_i^S\,dt \notag\\ &+ C\int_0^T \|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2\,dt + C(\delta_0+\varepsilon)\int_0^T \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx\,dt \notag\\ &+ C\int_0^T \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx\,dt + C\delta_0^{1/3}. \label{eq:weighted-gaussian} \end{align}\qquad{(48)}\]
Proof. Set \[\omega_G(t,x):=\frac{1}{\sqrt{1+t}}e^{-\frac{\beta |x|^2}{1+t}}, \quad h(t,x):=\int_{-\infty}^x \omega_G(t,y)\,dy, \quad H(t,x):=\int_{-\infty}^x \omega_G(t,y)^2\,dy .\] Then \[h_x=\omega_G,\qquad H_x=\omega_G^2,\qquad \omega_{Gt}=\frac{1}{4\beta}\omega_{Gxx},\qquad h_t=\frac{1}{4\beta}h_{xx},\] and \(h\), \(H\) are uniformly bounded on \([0,T]\times\mathbb{R}\).
We apply weighted multipliers directly to the macroscopic perturbation system 35 –36 . More precisely, we multiply the three momentum equations by \(\psi_i h^2\) \((i=1,2,3)\), and we combine the continuity equation 35 \(_1\) with the temperature equation 36 \(_2\) against \[H\Bigl(\frac{2}{3}\zeta-\bar p\,\phi\Bigr).\] After summing the resulting identities and integrating by parts in \(x\), the terms in which one derivative falls on \(H\) produce \(H_x=\omega_G^2\), hence yield the localized coercive quantity \[\int_{\mathbb{R}}\omega_G(t,x)^2\,|(\phi,\psi,\zeta)(t,x)|^2\,dx .\]
More precisely, one obtains \[\begin{align} \frac{d}{dt}\mathcal{J}_G(t) + c\int_{\mathbb{R}}\omega_G(t,x)^2\,|(\phi,\psi,\zeta)(t,x)|^2\,dx \le \mathcal{R}_G(t)+\mathcal{K}_G(t), \label{eq:WG-identity} \end{align}\tag{185}\] where \(\mathcal{J}_G(t)\) is a weighted interaction functional satisfying \[|\mathcal{J}_G(t)| \le C\|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 , \label{eq:WG-J-bound}\tag{186}\] \(\mathcal{R}_G(t)\) contains only macroscopic remainder terms, and \(\mathcal{K}_G(t)\) contains the microscopic moments coming from the \(\Pi_1\)-terms in 35 –36 .
We first estimate the macroscopic part. By construction, \(\mathcal{R}_G(t)\) is made of
(i) terms in which derivatives hit the weights \(h\) and \(H\);
(ii) the macroscopic error terms \(Q_1\), \(Q_2\), the profile interaction terms, and the modulation terms already treated in the zeroth-order analysis;
(iii) lower-order quadratic terms involving \((\phi_x,\psi_x,\zeta_x)\).
Since \(h\) and \(H\) are bounded, \(H_x=\omega_G^2\), and \[|\omega_{Gt}|+|h_t| \le C\left(\frac{1}{1+t}+\frac{|x|^2}{(1+t)^2}\right)\omega_G \le \frac{C}{1+t}\omega_G,\] all contributions of type (i) are bounded by \[C\sup_{t\in[0,T]}\|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 + C\int_0^T \|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2\,dt .\] For the terms of type (ii), we invoke the macroscopic zeroth-order structure already developed above: by 95 , the full collection of macroscopic error terms and lower-order shift contributions is controlled by \[C\sum_{i=1,3}\delta_i |\dot{X}_i|^2 + C\sum_{i=1,3}\mathcal{G}_i^S + C\delta_C\frac{1}{1+t}\int_{\mathbb{R}}e^{-2c|x|^2/(1+t)}|(\phi,\psi,\zeta)|^2\,dx + C\|(\phi_x,\psi_x,\zeta_x)\|_{L^2_x}^2 ,\] up to a harmless \(\lambda \mathcal{D}_{\mathrm{mac}}(U)\)-term, which we absorb by taking \(\lambda>0\) sufficiently small. The remaining pure profile terms are estimated by the Gaussian decay of the viscous contact wave and the exponential localization of the shock profiles, hence their time integrals are bounded by \(C\delta^{1/2}\) and the microscopic parts. More detail, we compute each Gaussian estiamtes as followed.
\[\begin{align} \label{eq:Gaussian1} & \left(\bar p \phi + \zeta \right)_t - \sum_{i\in\{1,3\}} \dot{X}_i \left( \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}} \bar p + \partial\bigl(\theta^{S_{i}}\bigr)^{-X_{i}} \right) + \bigl(p-\bar p\bigr)\psi_x \nonumber \\ & \quad = \bar p_t \phi - \bar u_x (p-\bar p)+\left(\alpha_{\rm {th}}(\theta)\frac{\theta_x}{v}-\alpha_{\rm{th}}(\bar \theta)\frac{\bar \theta_x}{\bar v}\right)_x \nonumber \\ & \qquad + \left(\mu(\theta)\frac{(u_x)^2}{v}-\mu(\bar \theta)\frac{(\bar u_x)^2}{\bar v}\right) - Q_2 + \frac{\mu(\theta)(\psi_{2x}^2 + \psi_{3x}^2)}{v} + K_{\theta} \end{align}\tag{187}\]
where
\[\begin{align} K_{\theta} :=& \sum_{j=2}^3 \psi_j \int \xi_1 \xi_j \Pi_{1x} d\xi - \int \xi_1 \frac{\left| \xi\right|^2}{2} \widetilde{\Pi}_{1x} d\xi \\ & \quad + u_1\int \xi_1^2 \Pi_{1x} d\xi - \sum_{i\in\{1,3\}} \bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\int \xi_1^2 \partial_x\bigl(\Pi_1^{S_{i}}\bigr)^{-X_{i}} d\xi. \end{align}\]
Take \(\mathcal{A}_G:=\bar p \phi + \zeta\) and observe that
\[\begin{align} \label{eq:Gaussian2} &\left[\mathcal{A}_G^2 \frac{h^2}{2}\right]_t - \frac{1}{4\beta}\mathcal{A}_G^2 h \omega_{Gx} - \sum_{i\in\{1,3\}} \dot{X}_i \left( \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}} \bar p + \partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}} \right) \mathcal{A}_G h^2 + \bigl(p-\bar p\bigr)\psi_x \mathcal{A}_G h^2 \nonumber \\ & = \left(\alpha_{\rm{th}}(\theta)\frac{\theta_x}{v}-\alpha_{\rm{th}}(\bar \theta)\frac{\bar \theta_x}{\bar v}\right)_x \mathcal{A}_G h^2 + \left[ \bar p_t \phi - \bar u_x (p-\bar p) + \left(\mu(\theta)\frac{(u_x)^2}{v}-\mu(\bar \theta)\frac{(\bar u_x)^2}{\bar v}\right) \nonumber\right. \\ & \left. \quad - Q_2 + \frac{\mu(\theta)(\psi_{2x}^2 + \psi_{3x}^2)}{v} + K_{\theta} \right] \mathcal{A}_G h^2 \end{align}\tag{188}\]
Applying the energy estimate to 188 ,
\[\begin{align} \label{eq:Gaussian3} &\frac{1}{4\beta} \int_0^T \int \mathcal{A}_G^2 \omega_G^2 dx dt = \int \mathcal{A}_G(0,x)^2 \frac{h_0^2}{2} dx \nonumber \\ &\quad - \int \mathcal{A}_G^2 \frac{h^2}{2} dx + \sum_{i\in\{1,3\}} \int_0^T \dot{X}_i \int \left( \partial_x \bigl(v^{S_{i}}\bigr)^{-X_{i}} \bar p + \partial_x \bigl(\theta^{S_{i}}\bigr)^{-X_{i}} \right) \mathcal{A}_G h^2 dx dt \nonumber \\ &\quad -\int_0^T\int \frac{1}{4\beta}(\mathcal{A}_G^2)_x h\omega_G dx dt -\int_0^T \int (p-\bar p)\psi_x \mathcal{A}_Gh^2 dx dt \nonumber\\ &\quad +\int_0^T \int \left[\bar p_t \phi -\bar u_x(p-\bar p) - Q_2 + \left(\mu(\theta)\frac{(u_x)^2}{v}-\mu(\bar \theta)\frac{(\bar u_x)^2}{\bar v}\right) \right] \mathcal{A}_Gh^2 dx dt \nonumber \\ &\quad -\int_0^T \int \left(\alpha_{\rm{th}}(\theta)\frac{\theta_x}{v}-\alpha_{\rm{th}}(\bar \theta)\frac{\bar \theta_x}{\bar v}\right) (\mathcal{A}_G h^2)_x dx dt +\int_0^T \int \left[\frac{\mu(\theta)(\psi_{2x}^2+\psi_{3x}^2)}{v}\right] \mathcal{A}_G h^2 dx dt \nonumber \\ &\quad +\int_0^T \int K_{\theta} \mathcal{A}_G h^2 dx dt =: \sum_{i=1}^9 J_i. \end{align}\tag{189}\]
See (D.16) in [37]. Then, \(J_i \, i=1,\ldots,7\) can be controlled as below.
\[\begin{align} \label{eq:Gaussian4} &\sum_{i=1}^7 J_i \le C \sup_{t\in[0,T]} \bigl\lVert(\phi,\zeta)\bigr\rVert_{L^2}^2 \nonumber\\ &\quad + C \sum_{i\in\{1,3\}} \delta_i \int_0^T \left| \dot{X}_i\right|^2 dt + (\nu+C\delta_0) \int_0^T \int \omega_G^2 \left| (\phi,\zeta)\right|^2 dx dt \nonumber\\ &\quad + C_{\nu} \int_0^T \bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 dt + C\sum_{i\in\{1,3\}}\int_0^T \mathcal{G}_i^S dt +C\delta_0^{\frac{1}{3}}. \end{align}\tag{190}\]
Since \(h\) is bounded, \(J_8\le C \int_0^T \bigl\lVert\psi_x\bigr\rVert^2_{L^2} dt\). The remain part \(J_9\) is purely kinetic term.
\[\begin{align} \label{eq:Gaussian5} &J_9 \le \int_0^T \iint (\zeta+\bar p \phi) \left[\sum_{j=2}^3 \psi_k \xi_1 \xi_j \Pi_{1x} \right] d\xi dx dt \nonumber \\ &\quad -\int_0^T \iint (\zeta+ \bar p \phi) \left[\xi_1 \frac{\left| \xi\right|^2}{2} \widetilde{\Pi}_{1x} d\xi\right] d\xi dx dt \nonumber \\ &\quad +\int_0^T \iint (\zeta+\bar p \phi)\left(u_1 \xi_1^2 \Pi_{1x} - \sum_{i\in\{1,3\}} \bigl(u_1^{S_{i}}\bigr)^{-X_{i}} \xi_1^2 \partial_x\bigl(\Pi_1^{S_{i}}\bigr)^{-X_{i}} \right) d\xi dx dt\\ &\qquad \quad =:J_{91}+J_{92}+J_{93}. \end{align}\tag{191}\]
By the similar argument of Lemma 19, we have the following bounds.
\[\begin{align} \label{eq:Gaussian6} &J_9 \le C(\delta_0+\varepsilon) \sum_{i\in\{1,3\}} \delta_i \int_0^T \left| \dot{X}_i\right|^2 dt + C\delta_0 \int_0^T \int \omega_G^2 \left| (\phi,\psi,\zeta)\right|^2 dx dt \nonumber\\ &\qquad + C \int_0^T \bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 dt + C\delta_0 \sum_{i\in\{1,3\}}\int_0^T \mathcal{G}_i^S dt \nonumber\\ &\qquad + C(\delta_0+\varepsilon)\int_0^T \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\, dx \,dt \nonumber\\ &\qquad + C\int_0^T \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \, dx\, dt +C\delta_0^{\frac{1}{3}}. \end{align}\tag{192}\]
Also, we can apply to \(H(\frac{2}{3}\zeta-\bar \phi)\) (\(\mathcal{B}_G:=\frac{2}{3}\zeta-\bar \phi\)) by the similar argument, we have the following estimate.
\[\begin{align} \label{eq:Gaussian7} & \int_0^T \int \omega_G^2 \left[\frac{1}{2v}\mathcal{B}_G^2 + \frac{4\bar p |\psi_1|^2}{3}\right] dx dt = \int H\psi_1\mathcal{B}_G|_{t=0}^{t=T} dx \nonumber \\ & \quad + \int_0^T \int v_x \frac{H}{2v^2}\mathcal{B}_G^2 dx dt - \int_0^T \int \psi\mathcal{B}_G H_t dx dt \nonumber \\ & \quad + \sum_{i\in\{1,3\}}\int_0^T \dot{X}_i \int H \left[\bar p \psi \partial_x\bigl(v^{S_{i}}\bigr)^{-X_{i}} -\psi \partial_x\bigl(\theta^{S_{i}}\bigr)^{-X_{i}} - \mathcal{B}_G \partial_x\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right] dx dt \nonumber\\ & \quad -\int_0^T \int \bar p_x H \frac{4}{3}\psi_1^2 dx dt +\int_0^T \int \frac{2}{3} H \psi\left[(p-\bar p)\psi_x+\bar u_x(p-\bar p)\right] dx dt \nonumber\\ & \quad +\int_0^T \int H\psi \phi \bar p_t dx dt + \int_0^T \int \frac{2}{3}H\psi_1 \left(\mu(\theta)\frac{u_{1x}^2}{v}-\mu(\bar{\theta})\frac{(\bar u_{1x})^2}{\bar v}\right) dx dt \nonumber\\ & \quad +\int_0^T \int \left(H\mathcal{B}_G\right)_x\left(\mu(\theta)\frac{u_x}{v}-\mu(\overline{\theta})\frac{\bar u_x}{\bar v}\right) dx dt \nonumber \\ & \quad+ \int_0^T \int \frac{2}{3} (H\psi)_x\left(\alpha_{\rm{th}}(\theta)\frac{\theta_x}{v}-\alpha_{\rm{th}}(\bar \theta)\frac{\bar \theta_x}{\bar v}\right) dx dt + \int_0^T \int \left[\frac{2}{3}HQ_2 + H\mathcal{B}_GQ_1\right] dx dt \nonumber\\ &\quad + \int_0^T \int \left[\frac{2}{3} H K_\theta + H\mathcal{B}_G K_u\right] dx dt \end{align}\tag{193}\] where \[\begin{align} K_u:= -\int \xi_1^2 \widetilde{\Pi}_{1x} d\xi. \end{align}\]
By using the result of [37] and Lemma 19, we have
\[\begin{align} \label{eq:Gaussian8} & \int_0^T \int \omega_G^2 \left[\frac{1}{2v}\mathcal{B}_G^2 + \frac{4\bar p |\psi_1|^2}{3}\right] dx dt \le C \sup_{t\in[0,T]} \bigl\lVert(\phi,\psi,\zeta)\bigr\rVert_{L^2}^2 \nonumber\\ &\quad + C \sum_{i\in\{1,3\}} \delta_i \int_0^T \left| \dot{X}_i\right|^2 dt + C \delta_0 \int_0^T \int \omega_G^2 \left| (\phi,\psi,\zeta)\right|^2 dx dt \nonumber\\ &\quad + C \int_0^T \bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 dt + C(\delta_0+\varepsilon)\sum_{i\in\{1,3\}}\int_0^T \mathcal{G}_i^S dt \nonumber\\ &\qquad + C(\delta_0+\varepsilon)\int_0^T \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\, dx\, dt \nonumber\\ &\qquad + C\int_0^T \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx\, dt +C\delta_0^{\frac{1}{3}}. \end{align}\tag{194}\]
Finally, consider the \(\psi_{i},\, i=2,3\) cases. Multiply to 36 by \(\psi_ih^2\). \[\begin{align} \label{eq:Gaussian9} h^2\psi_i\psi_{it} = h^2\psi_i\left(\frac{\mu(\theta)\psi_{ix}}{v}\right)_x - h^2 \int \psi_i \xi_1 \xi_i \Pi_{1x} d\xi. \end{align}\tag{195}\]
Note that \[\begin{align} (\psi_i^2 \frac{h^2}{2})_t =& h^2\psi_i\psi_{it} + \frac{1}{4\beta}\omega_{Gx} \psi_i^2\\ =& h^2\psi_i\psi_{it} + \left[\frac{1}{4\beta}\psi_i^2 h \omega_G\right]_x -\frac{1}{4\beta}\psi_i^2 \omega_G^2 -\frac{1}{4\beta} (\psi_i^2)_x h \omega_G. \end{align}\]
Therefore, \[\begin{align} \label{eq:Gaussian10} &\frac{1}{4\beta}\int_0^T\int \psi_i^2 \omega_G^2 dx dt = \int \psi_i(0,x)^2 \frac{h_0^2}{2} dx \nonumber\\ &\qquad -\int \psi_i^2 \frac{h^2}{2}dx -\int_0^T \int \frac{1}{4\beta} (\psi_i^2)_x h\omega_G dx dt \nonumber \\ &\qquad - \int_0^T (\psi_i^2 h)_x \frac{\mu(\theta)\psi_{ix}}{v} dx dt - \int_0^T h^2 \int K_{gi} dx dt \end{align}\tag{196}\] where \[\begin{align} K_{gi}:= -\int \psi_i\xi_1 \xi_i \Pi_{1x} d\xi. \end{align}\]
By using Lemma 19, we have the following estimate.
\[\begin{align} \label{eq:Gaussian11} &\int_0^T\int \psi_i^2 \omega_G^2 dx dt \le C \sup_{t\in[0,T]} \bigl\lVert(\phi,\psi,\zeta)\bigr\rVert_{L^2}^2 \nonumber\\ &\qquad + C \sum_{i\in\{1,3\}} \delta_i \int_0^T \left| \dot{X}_i\right|^2 dt + C \delta_0 \int_0^T \int W^2 \left| (\phi,\psi,\zeta)\right|^2 dx dt \nonumber\\ &\qquad + C \int_0^T \bigl\lVert(\phi_x,\psi_x,\zeta_x)\bigr\rVert_{L^2}^2 dt + C(\delta_0+\varepsilon)\sum_{i\in\{1,3\}}\int_0^T \mathcal{G}_i^S dt \nonumber\\ &\qquad + C(\delta_0+\varepsilon)\int_0^T \int \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx \,dt \nonumber\\ &\qquad + C\int_0^T \int \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2+\bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 d\xi dx dt +C\delta_0^{\frac{1}{3}}. \end{align}\tag{197}\]
Collecting 190 , 192 , 194 , and 197 , Lemma 41 was proved. ◻
Proof of Proposition 1. We combine the zeroth-order estimate from Section 6, the differentiated estimates from Section 7, and the Gaussian-weighted estimate of Lemma 41.
For \(t\in[0,T]\), let \(\mathfrak{R}(t)^2\) denote the full left-hand side of ?? , with \(T\) replaced by \(t\). Since ?? does not explicitly contain the first-order time derivatives, we also introduce the auxiliary quantity \[\mathcal{E}_t(t)^2 := \int_0^t \|(\phi_t,\psi_t,\zeta_t)(s)\|_{L^2_x}^2\,ds .\] It is enough to prove \[\mathfrak{R}(t)^2+\mathfrak T(t)^2 \le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr), \qquad 0\le t\le T.\]
We also set \[\mathcal{W}_C(t) := \int_0^t \frac{1}{1+s}\int_{\mathbb{R}} e^{-\frac{2c|x|^2}{1+s}}|(\phi,\psi,\zeta)(s,x)|^2\,dx\,ds ,\] and \[\mathcal{K}(t) := \int_0^t\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx\,ds + \mathcal{K}_{\mathrm{high}}(t).\]
Step 1: Zeroth-order control. By Lemma 23, more precisely by ?? , the weighted relative entropy is equivalent to the \(L^2_x\)-norm of the macroscopic perturbation. In addition, 130 identifies the zeroth-order energy with \[\|(\phi,\psi,\zeta)(t)\|_{L^2_x}^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{M_\#}^2\,dx .\] Moreover, by the definition of the dissipation \(\mathcal{D}_{\mathrm{mac}}(U)\) in 86 , together with the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 , one has \[\mathcal{D}_{\mathrm{mac}}(U)(t)\ge c\,\|(\psi_x,\zeta_x)(t)\|_{L^2_x}^2 .\] Therefore Proposition 6, namely ?? , yields \[\begin{align} \begin{aligned} &\sup_{0\le s\le t} \left\{ \|(\phi,\psi,\zeta)(s)\|_{L^2_x}^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{M_\#}^2\,dx \right\} \\ &\quad + \int_0^t \sum_{i=1,3}\delta_i |\dot{X}_i(s)|^2\,ds + \int_0^t \sum_{i=1,3}\mathcal{G}_i^S(s)\,ds + \int_0^t \|(\psi_x,\zeta_x)(s)\|_{L^2_x}^2\,ds \\ &\quad + \int_0^t\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx\,ds \\ &\le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr) + C\delta_C\mathcal{W}_C(t) + C\int_0^t\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 \,dx\,ds . \end{aligned} \label{eq:priest-step1} \end{align}\tag{198}\]
Step 2: The low-order differentiated estimate. We next integrate ?? over \([0,t]\). The energy functional there contains the cross term \(\int_{\mathbb{R}} v\psi_1\phi_x\,dx\), but by the bootstrap bound \(\mathcal{E}(T)^2\le \varepsilon^2\) in 44 and Young’s inequality, \[\left|\int_{\mathbb{R}} v\psi_1\phi_x\,dx\right| \le \frac{1}{4}\|\phi_x\|_{L^2_x}^2 + C\|\psi_1\|_{L^2_x}^2 ,\] and the \(L^2_x\)-norm of \(\psi_1\) is already controlled by 198 . Using also the bound for \(\int_0^t \|(\psi_x,\zeta_x)(s)\|_{L^2_x}^2\,ds\) furnished by 198 , we obtain \[\begin{align} \begin{aligned} &\sup_{0\le s\le t} \left\{ \|\phi_x(s)\|_{L^2_x}^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{M_\#}^2 \,dx \right\} + \mathcal{E}_t(t)^2 \\ &\quad + \int_0^t\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2\,dx\,ds \\ &\le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr) + C\varepsilon^2\int_0^t \|\psi_{1xx}(s)\|_{L^2_x}^2\,ds + C\delta_C \mathcal{W}_C(t) + C\mathcal{K}_{\mathrm{high}}(t). \end{aligned} \label{eq:priest-step2} \end{align}\tag{199}\]
Step 3: High-order closure. We now invoke Proposition 7, namely ?? . This estimate provides the remaining first-order spatial derivatives \((\psi_x,\zeta_x)\), the second-order macroscopic terms \[(\phi_{xx},\psi_{xx},\zeta_{xx},\phi_{xt},\psi_{xt},\zeta_{xt}),\] and the differentiated microscopic quantities \[\widetilde{G}_x,\qquad \widetilde{G}_t,\qquad \widetilde{G}_{xx},\qquad \widetilde{G}_{xt}.\] Its right-hand side depends only on lower-order quantities, namely \[\int_0^t \sum_{i=1,3}\delta_i |\dot{X}_i|^2\,ds,\qquad \int_0^t \sum_{i=1,3}\mathcal{G}_i^S\,ds,\qquad \int_0^t \sum_{|\beta|=1}\|\partial^\beta(\phi,\psi,\zeta)\|_{L^2_x}^2\,ds,\] and \[\int_0^t\int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{\text{rem}}\bigr\rVert_{\nu,M_\#}^2 \,dx\,ds ,\] which are precisely the quantities controlled by 198 and 199 . Therefore \[\begin{align} \begin{aligned} &\sup_{0\le s\le t} \left\{ \|(\phi_x,\psi_x,\zeta_x)(s)\|_{L^2_x}^2 + \int_{\mathbb{R}} \bigl\lVert\widetilde{G}_{x}\bigr\rVert_{M_\#}^2+\bigl\lVert\widetilde{G}_{t}\bigr\rVert_{M_\#}^2+\bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{M_\#}^2+\bigl\lVert\widetilde{G}_{tx}\bigr\rVert_{M_\#}^2 \,dx \right\} \\ &\quad + \int_0^t \|(\phi_{xx},\psi_{xx},\zeta_{xx},\phi_{xt},\psi_{xt},\zeta_{xt})(s)\|_{L^2_x}^2\,ds \\ &\quad + \int_0^t\mathcal{K}_{\mathrm{high}}(s)\,ds \\ &\le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr) + C\delta_C\mathcal{W}_C(t) + C(\delta_0+\varepsilon)\bigl(\mathfrak{R}(t)^2+\mathcal{E}_t(t)^2\bigr). \end{aligned} \label{eq:priest-step3} \end{align}\tag{200}\]
Step 4: Control of the Gaussian-weighted term. We now apply Lemma 41 on the interval \([0,t]\). Since the right-hand side of ?? contains only the lower-order quantities already controlled by 198 , 199 , and 200 , we obtain \[\delta_C\mathcal{W}_C(t) \le C\delta_C\bigl(\mathcal{E}(0)^2+\delta_0^{1/3}\bigr) + C\delta_C(\delta_0+\varepsilon)\bigl(\mathcal{E}(t)^2+\mathfrak T(t)^2\bigr). \label{eq:priest-step4}\tag{201}\]
Step 5: Final absorption. Combining 198 , 199 , 200 , and 201 , we find \[\mathfrak{R}(t)^2+\mathcal{E}_t(t)^2 \le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr) + C\varepsilon^2\int_0^t \|\psi_{1xx}(s)\|_{L^2_x}^2\,ds + C(\delta_0+\varepsilon)\bigl(\mathfrak{R}(t)^2+\mathcal{E}_t(t)^2\bigr).\] Since \(\int_0^t \|\psi_{1xx}(s)\|_{L^2_x}^2\,ds\) is already one of the components of \(\mathfrak{R}(t)^2\), it follows that \[\mathfrak{R}(t)^2+\mathcal{E}_t(t)^2 \le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr) + C(\delta_0+\varepsilon)\bigl(\mathfrak{R}(t)^2+\mathcal{E}_t(t)^2\bigr).\] Choosing \(\delta_0>0\) and \(\varepsilon>0\) sufficiently small, we absorb the last term into the left-hand side and conclude that \[\mathfrak{R}(t)^2+\mathcal{E}_t(t)^2 \le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr), \qquad 0\le t\le T.\] In particular, \[\mathfrak{R}(t)^2 \le C\bigl(\mathcal{E}(0)^2+\delta_0^{1/2}\bigr), \qquad 0\le t\le T.\] Taking \(t=T\), and recalling the definition of \(\mathfrak{R}(T)^2\), we obtain exactly ?? . This proves Proposition 1. ◻
In this subsection, we specialize the analysis to the case where the background profile consists of a single shifted Boltzmann shock profile only. Accordingly, there is no contact wave, no second shock component, and no wave interaction.
Theorem 3 (Away-from-the-shock convergence in \(L^\infty_x\) for a single shock). Assume that the hypotheses of Proposition 8 hold. Then, for every \(T>0\), there exist positive constants \(C\) and \(c\), independent of \(\kappa\in(0,\kappa_0]\), such that for all \((\tau,y)\in[0,T]\times\mathbb{R}\), \[\begin{align} \left\| f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \le C\,\kappa + C e^{-c|y-s\tau-X^\kappa(\tau)|/\kappa}. \label{eq:single-shock-away-pointwise} \end{align}\qquad{(49)}\]
Let \[\bar U(t,x)=U^S(x-st-X(t)) = (\bar v,\bar u,\bar\theta)(t,x)\] be the shifted single shock profile, where \(U^S\) is the monotone Boltzmann 3-shock profile, \(s=\sigma\) is the shock speed and \(X(t)\) is the modulation shift. In analogy with the weighted entropy construction in the composite-wave case, we introduce the single-shock weight \[a^{\mathrm{sh}}(t,x) := 1+\frac{1}{\sqrt{\delta}}\bigl(\bar v(t,x)-v_-\bigr), \label{eq:single-shock-weight}\tag{202}\] where \[\delta:=|v_+-v_-|\] denotes the shock strength.
\[\begin{align} p_- = \frac{2\theta_-}{3v_-},\quad \sigma_- = \sqrt{\frac{5p_-}{3v_-}}. \end{align}\]
These constants are chosen according to the admissible range of the shock strengths and the associated shock speeds, and they will be used in the definition of the coefficient \(\mathfrak m\) below. We now define the dynamical shift \(X\) by the system of ordinary differential equations \[\label{eq:shifts} \begin{align} \dot{X}(t) &= -\frac{\mathfrak m}{\delta} \int_{\mathbb{R}} a^{\mathrm{sh}} \left( \left((u_1^{S})^{-X}\right)_x\psi_1 + \frac{\left((v^{S})^{-X}\right)_x\,\overline{p}}{\overline{v}}\phi + \frac{\left((\theta^{S})^{-X}\right)_x}{\overline{\theta}}\zeta \right)\,dx,\\ X(0)&=0, \end{align}\tag{203}\] where the constant \(\mathfrak m\) is defined as below. \[\begin{align} \label{eq:ssm} \mathfrak m:=\frac{20}{3}\frac{p_-}{(\sigma_-)^3(v_-)^2}\frac{5+3\gamma}{10+3\gamma}. \end{align}\tag{204}\]
We define the associated single-shock coercive quantity by \[\mathcal{G}_{\mathrm{sh}}(t) := \int_{\mathbb{R}}\bigl|\bar v_x(t,x)\bigr|\, |(\phi,\psi,\zeta)(t,x)|^2\,dx . \label{eq:def-Gsh}\tag{205}\]
We first record the single-shock analogue of the main a priori estimate. Its proof is obtained by combining the zeroth-order estimate, the low-order differentiated estimate, and the high-order closure, exactly as in the composite-wave case, but with all contact-generated and interaction-generated remainders removed.
Proposition 8 (Main a priori estimate for a single 3-shock). Assume that the background profile consists of a single shifted Boltzmann shock profile only. Then there exist positive constants \(\delta_0\), \(\varepsilon\), and \(C\), together with a global Maxwellian \(M_\#:=M[U_\#]\), such that the following holds.
Suppose that \((U,f)=(v,u,\theta,f)\) solves the perturbation system around the single shifted shock profile on \([0,T]\), with modulation \(X(t)\), and assume that \[\delta\in(0,\delta_0), \qquad \mathcal{E}(T)^2\le \varepsilon^2 .\] Then \[\begin{align} \begin{aligned} \mathcal{E}(T)^2 &+\int_0^T \delta |\dot{X}(t)|^2\,dt +\int_0^T \mathcal{G}_{\mathrm{sh}}(t)\,dt +\sum_{|\beta|=1}\int_0^T \|\partial^\beta(\phi,\psi,\zeta)(t)\|_{L^2_x}^2\,dt \\ &\quad +\int_0^T \|(\phi_{xx},\psi_{xx},\zeta_{xx},\phi_{xt},\psi_{xt},\zeta_{xt})(t)\|_{L^2_x}^2\,dt \\ &\quad +\int_0^T\int_{\mathbb{R}} \bigl\lVert\widetilde{G}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xx}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{xt}\bigr\rVert_{\nu,M_\#}^2 \,dx\,dt \\ &\le C\,\mathcal{E}(0)^2 . \end{aligned} \label{eq:pries-single} \end{align}\qquad{(50)}\] Here \(\mathcal{G}_{\mathrm{sh}}(t)\) is the single-shock coercive quantity defined in 205 .
Proof. For a single 3-shock, we set \(\delta_1=\delta_C=0\). Then the interaction estimates, as well as the error terms generated by the cutoff functions \(\varphi_i\) (See 41 ) introduced to separate the two shocks in the a-priori estimates ?? , disappear. In particular, the term \(\delta_0^{1/2}\) on the right hand side of the composite-wave a priori estimate ?? from the wave interactions, and therefore it is absent in the single-shock case. In addition, the zeroth perturbed microscopic variable \(\widetilde{G}_{\mathrm{rem}}=\widetilde{G} = G-\bigl(G^S\bigr)^{-X}\) since there is no contact discontinuity. All the remaining estimates follow directly from the estimates established in the previous section. ◻
Lemma 42 (Exponential localization of the single shock profile). Let \[F^{S}(z,\xi)=M[U^{S}](z,\xi)+G^{S}(z,\xi)\] be the single Boltzmann shock profile connecting the end Maxwellians \[M_-:=M[U_-], \qquad M_+:=M[U_+].\] Assume that \(F^S\) is smooth and converges exponentially to its end states. Then there exist positive constants \(C\) and \(c\) such that \[\begin{align} \|F^{S}(z,\cdot)-M_\pm\|_{M_\#} + |U^{S}(z)-U_\pm| \le Ce^{-c|z|}, \qquad \pm z\ge0 . \label{eq:single-shock-tail-basic} \end{align}\qquad{(51)}\]
Let the shifted \(\kappa\)-shock profile be defined by \[\bar f^\kappa(\tau,y,\xi) := F^{S}\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right),\] and let the associated modulated Euler Maxwellian be \[M_{E,\kappa}(\tau,y,\xi) := \begin{cases} M_-(\xi), & y\le s\tau+X^\kappa(\tau),\\[2mm] M_+(\xi), & y> s\tau+X^\kappa(\tau). \end{cases}\] Then for every \(T>0\), the pointwise bound \[\begin{align} \left\| \bar f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \le Ce^{-c|y-s\tau-X^\kappa(\tau)|/\kappa} \label{eq:single-shock-tail-pointwise} \end{align}\qquad{(52)}\] holds for all \((\tau,y)\in[0,T]\times\mathbb{R}\). In particular, for every \(h>0\), \[\begin{align} \sup_{\substack{0\le \tau\le T\\ |y-s\tau-X^\kappa(\tau)|\ge h}} \left\| \bar f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \le Ce^{-ch/\kappa}. \label{eq:single-shock-tail-scaled} \end{align}\qquad{(53)}\]
Proof. The estimate ?? is precisely the exponential convergence of the travelling shock profile to its end Maxwellians.
To prove the pointwise estimate ?? , fix \((\tau,y)\in[0,T]\times\mathbb{R}\), and set \[z:=\frac{y-s\tau-X^\kappa(\tau)}{\kappa}.\] Then \[\bar f^\kappa(\tau,y,\xi)=F^S(z,\xi).\]
If \(z\le0\), then by the definition of \(M_{E,\kappa}\), \[M_{E,\kappa}(\tau,y,\xi)=M_-(\xi),\] and therefore, using ?? with the minus sign, \[\left\| \bar f^\kappa(\tau,y,\cdot)-M^{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} = \|F^S(z,\cdot)-M_-\|_{M_\#} \le Ce^{-c|z|}.\]
If \(z>0\), then \[M_{E,\kappa}(\tau,y,\xi)=M_+(\xi),\] and ?? with the plus sign gives \[\left\| \bar f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} = \|F^S(z,\cdot)-M_+\|_{M_\#} \le Ce^{-c|z|}.\]
Since \[|z|=\frac{|y-s\tau-X^\kappa(\tau)|}{\kappa},\] the two cases combine to yield ?? .
Finally, if \[|y-s\tau-X^\kappa(\tau)|\ge h,\] then ?? implies \[\left\| \bar f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \le Ce^{-ch/\kappa}.\] Taking the supremum over all such \((\tau,y)\) gives ?? . ◻
Proof of Theorem 3. For the single-shock problem, define \[\bar U^\kappa(\tau,y) := U^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa}\right), \qquad \bar M^\kappa(\tau,y,\xi) := M[\bar U^\kappa(\tau,y)](\xi),\] and \[\bar f^\kappa(\tau,y,\xi) := F^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right).\] By the decomposition \(F^S=M[U^S]+G^S\), we have \[\bar f^\kappa(\tau,y,\xi) = \bar M^\kappa(\tau,y,\xi) + G^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right).\]
Let \[U^\kappa=(v^\kappa,u^\kappa,\theta^\kappa), \qquad (\phi^\kappa,\psi^\kappa,\zeta^\kappa) := U^\kappa-\bar U^\kappa .\] Hence \[f^\kappa-\bar f^\kappa = \bigl(M[U^\kappa]-\bar M^\kappa\bigr) + \widetilde{G}^\kappa . \label{eq:single-shock-away-pointwise-decomp}\tag{206}\]
By Proposition 8, for every fixed \(T>0\), \[\mathcal{E}^\kappa(T)^2\le C\,\mathcal{E}^\kappa(0)^2 .\] Recalling the definition of \(\mathcal{E}^\kappa(T)\), and using \(\widetilde{G}^\kappa=\widetilde{G}_1^\kappa\), we infer that \[\sup_{0\le\tau\le T} \|(\phi^\kappa,\psi^\kappa,\zeta^\kappa)(\tau)\|_{H^1_y} \le C\,\mathcal{E}^\kappa(0), \label{eq:single-shock-away-H1-fluid}\tag{207}\] and \[\sup_{0\le\tau\le T} \|\widetilde{G}_1^\kappa(\tau,\cdot,\cdot)\|_{H^1_y(L^2_\xi(M_\#))} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-H1-micro}\tag{208}\]
Applying Lemma 46 with \(H=\mathbb{R}^3\) to \((\phi^\kappa,\psi^\kappa,\zeta^\kappa)\), and with \(H=L^2_\xi(M_\#^{-1})\) to \(\widetilde{G}^\kappa\), we obtain \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} |U^\kappa(\tau,y)-\bar U^\kappa(\tau,y)| \le C\,\mathcal{E}^\kappa(0), \label{eq:single-shock-away-Linfty-fluid}\tag{209}\] and \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|\widetilde{G}^\kappa(\tau,y,\cdot)\|_{M_\#} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-Linfty-micro}\tag{210}\]
Next we compare the Maxwellian parts. Since the single shock profile \(U^S\) connects the fixed end states \(U_-\) and \(U_+\), its range is contained in a compact set \[K_S\Subset \mathbb{R}_+\times\mathbb{R}\times\mathbb{R}_+ .\] By 209 , and after possibly shrinking the bootstrap constant \(\kappa_0\), the range of \(U^\kappa\) on \([0,T]\times\mathbb{R}\) is contained in a fixed compact set \[K\Subset \mathbb{R}_+\times\mathbb{R}\times\mathbb{R}_+\] depending only on \(K_S\) and \(\kappa_0\). Therefore Lemma 47 applies uniformly on \(K\), and yields \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|M[U^\kappa(\tau,y)]-\bar M^\kappa(\tau,y)\|_{M_\#} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-Maxwellian}\tag{211}\]
Combining 206 , 210 , and 211 , we obtain the uniform estimate \[\|f^\kappa(\tau,y,\cdot)-\bar f^\kappa(\tau,y,\cdot)\|_{M_\#} \le C\,\mathcal{E}^\kappa(0), \qquad (\tau,y)\in[0,T]\times\mathbb{R}. \label{eq:single-shock-away-pointwise-step1}\tag{212}\]
On the other hand, Lemma 42 gives the pointwise exponential tail estimate \[\|\bar f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot)\|_{M_\#} \le C e^{-c|y-s\tau-X^\kappa(\tau)|/\kappa}, \qquad (\tau,y)\in[0,T]\times\mathbb{R}. \label{eq:single-shock-away-pointwise-step2}\tag{213}\]
Therefore, by the triangle inequality,
\[\begin{align} & \left\| f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \\ &\quad \le \left\| f^\kappa(\tau,y,\cdot)-\bar f^\kappa(\tau,y,\cdot) \right\|_{M_\#} + \left\| \bar f^\kappa(\tau,y,\cdot)-M_{E,\kappa}(\tau,y,\cdot) \right\|_{M_\#} \\ &\quad \le C\,\mathcal{E}^\kappa(0) + C e^{-c|y-s\tau-X^\kappa(\tau)|/\kappa}\\ &\quad \le C\, \kappa \mathcal{E}(0) + C e^{-c|y-s\tau-X^\kappa(\tau)|/\kappa} \end{align}\]
which proves ?? . ◻
Proof of Theorem 3. For the single-shock problem, define \[\bar U^\kappa(\tau,y) := U^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa}\right), \qquad \bar M^\kappa(\tau,y,\xi) := M[\bar U^\kappa(\tau,y)](\xi),\] and \[\bar f^\kappa(\tau,y,\xi) := F^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right).\] Then \[\bar f^\kappa(\tau,y,\xi) = \bar M^\kappa(\tau,y,\xi) + G^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right).\]
Let \[U^\kappa=(v^\kappa,u^\kappa,\theta^\kappa), \qquad (\phi^\kappa,\psi^\kappa,\zeta^\kappa) := U^\kappa-\bar U^\kappa .\] Since there is no contact component in the present setting, \[\widetilde{G}_0^\kappa\equiv0, \qquad \widetilde{G}^\kappa=\widetilde{G}_1^\kappa,\] and therefore \[f^\kappa-\bar f^\kappa = \bigl(M[U^\kappa]-\bar M^\kappa\bigr) + \widetilde{G}_1^\kappa . \label{eq:single-shock-away-pointwise-decomp1}\tag{214}\]
By Proposition 8, for every fixed \(T>0\), \[\mathcal{E}^\kappa(T)^2\le C\,\mathcal{E}^\kappa(0)^2.\] Hence \[\sup_{0\le\tau\le T} \|(\phi^\kappa,\psi^\kappa,\zeta^\kappa)(\tau)\|_{H^1_y} \le C\,\mathcal{E}^\kappa(0),\] and \[\sup_{0\le\tau\le T} \|\widetilde{G}_1^\kappa(\tau,\cdot,\cdot)\|_{H^1_y(L^2_\xi(M_\#^{-1}))} \le C\,\mathcal{E}^\kappa(0).\] By Lemma 46, it follows that \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} |U^\kappa(\tau,y)-\bar U^\kappa(\tau,y)| \le C\,\mathcal{E}^\kappa(0),\] and \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|\widetilde{G}_1^\kappa(\tau,y,\cdot)\|_{L^2_\xi(M_\#^{-1})} \le C\,\mathcal{E}^\kappa(0).\] By the local Lipschitz continuity of the Maxwellian map on compact positive sets, \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|M[U^\kappa(\tau,y)]-\bar M^\kappa(\tau,y)\|_{L^2_\xi(M_\#^{-1})} \le C\,\mathcal{E}^\kappa(0).\] Combining these bounds with 214 , we obtain the uniform estimate \[\|f^\kappa(\tau,y,\cdot)-\bar f^\kappa(\tau,y,\cdot)\|_{L^2_\xi(M_\#^{-1})} \le C\,\mathcal{E}^\kappa(0), \qquad (\tau,y)\in[0,T]\times\mathbb{R}. \label{eq:single-shock-away-pointwise-step1-1}\tag{215}\]
Next, Lemma 42 gives the pointwise exponential tail estimate \[\|\bar f^\kappa(\tau,y,\cdot)-M^{E,\kappa}(\tau,y,\cdot)\|_{L^2_\xi(M_\#^{-1})} \le C e^{-c|y-s\tau-X^\kappa(\tau)|/\kappa}, \qquad (\tau,y)\in[0,T]\times\mathbb{R}. \label{eq:single-shock-away-pointwise-step2-1}\tag{216}\]
Therefore, by the triangle inequality, \[\begin{align} \left\| f^\kappa(\tau,y,\cdot)-M^{E,\kappa}(\tau,y,\cdot) \right\|_{L^2_\xi(M_\#^{-1})} &\le \left\| f^\kappa(\tau,y,\cdot)-\bar f^\kappa(\tau,y,\cdot) \right\|_{L^2_\xi(M_\#^{-1})} \\ &\quad + \left\| \bar f^\kappa(\tau,y,\cdot)-M^{E,\kappa}(\tau,y,\cdot) \right\|_{L^2_\xi(M_\#^{-1})} \\ &\le C\,\mathcal{E}^\kappa(0) + C e^{-c|y-s\tau-X^\kappa(\tau)|/\kappa}, \end{align}\] which proves ?? .
Finally, if \((\tau,y)\in\Omega^\kappa_{h,T}\), then \[|y-s\tau-X^\kappa(\tau)|\ge h,\] so ?? immediately yields [eq:single-shock-away-modulated]. ◻
Proof of Theorem 3. For the single-shock problem, define \[\bar U^\kappa(\tau,y) := U^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa}\right), \qquad \bar M^\kappa(\tau,y,\xi) := M[\bar U^\kappa(\tau,y)](\xi),\] and \[\bar f^\kappa(\tau,y,\xi) := F^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right).\] Then \[\bar f^\kappa(\tau,y,\xi) = \bar M^\kappa(\tau,y,\xi) + G^S\!\left(\frac{y-s\tau-X^\kappa(\tau)}{\kappa},\xi\right).\]
Let \[U^\kappa=(v^\kappa,u^\kappa,\theta^\kappa)\] denote the macroscopic field associated with \(f^\kappa\), and set \[(\phi^\kappa,\psi^\kappa,\zeta^\kappa) := U^\kappa-\bar U^\kappa .\] Since there is no contact component in the present setting, we have \[\widetilde{G}_0^\kappa\equiv0, \qquad \widetilde{G}^\kappa=\widetilde{G}_1^\kappa .\] Hence \[f^\kappa-\bar f^\kappa = \bigl(M[U^\kappa]-\bar M^\kappa\bigr) + \widetilde{G}_1^\kappa . \label{eq:single-shock-away-decomp}\tag{217}\]
By Proposition 8, for every fixed \(T>0\), \[\mathcal{E}^\kappa(T)^2\le C\,\mathcal{E}^\kappa(0)^2 .\] Recalling the definition of \(\mathcal{E}^\kappa(T)\), and using \(\widetilde{G}^\kappa=\widetilde{G}_1^\kappa\), we infer that \[\sup_{0\le\tau\le T} \|(\phi^\kappa,\psi^\kappa,\zeta^\kappa)(\tau)\|_{H^1_y} \le C\,\mathcal{E}^\kappa(0), \label{eq:single-shock-away-H1-fluid1}\tag{218}\] and \[\sup_{0\le\tau\le T} \|\widetilde{G}_1^\kappa(\tau,\cdot,\cdot)\|_{H^1_y(L^2_\xi(M_\#^{-1}))} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-H1-micro1}\tag{219}\]
Applying Lemma 46 with \(H=\mathbb{R}^3\) to \((\phi^\kappa,\psi^\kappa,\zeta^\kappa)\), and with \(H=L^2_\xi(M_\#^{-1})\) to \(\widetilde{G}_1^\kappa\), we obtain \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} |U^\kappa(\tau,y)-\bar U^\kappa(\tau,y)| \le C\,\mathcal{E}^\kappa(0), \label{eq:single-shock-away-Linfty-fluid1}\tag{220}\] and \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|\widetilde{G}_1^\kappa(\tau,y,\cdot)\|_{L^2_\xi(M_\#^{-1})} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-Linfty-micro1}\tag{221}\]
Next we compare the Maxwellian parts. Since the single shock profile \(U^S\) connects the fixed end states \(U_-\) and \(U_+\), its range is contained in a compact set \[K_S\Subset \mathbb{R}_+\times\mathbb{R}\times\mathbb{R}_+ .\] By 220 , and after possibly shrinking the bootstrap constant \(\kappa_0\), the range of \(U^\kappa\) on \([0,T]\times\mathbb{R}\) is contained in a fixed compact set \[K\Subset \mathbb{R}_+\times\mathbb{R}\times\mathbb{R}_+\] depending only on \(K_S\) and \(\kappa_0\). Therefore Lemma 47 applies uniformly on \(K\), and yields \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|M[U^\kappa(\tau,y)]-\bar M^\kappa(\tau,y)\|_{L^2_\xi(M_\#^{-1})} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-Maxwellian1}\tag{222}\]
Combining 217 , 221 , and 222 , we obtain \[\sup_{0\le\tau\le T}\sup_{y\in\mathbb{R}} \|f^\kappa(\tau,y,\cdot)-\bar f^\kappa(\tau,y,\cdot)\|_{L^2_\xi(M_\#^{-1})} \le C\,\mathcal{E}^\kappa(0). \label{eq:single-shock-away-step1}\tag{223}\]
On the other hand, Lemma 42 yields \[\sup_{(\tau,y)\in\Omega^\kappa_{h,T}} \|\bar f^\kappa(\tau,y,\cdot)-M^{E,\kappa}(\tau,y,\cdot)\|_{L^2_\xi(M_\#^{-1})} \le Ce^{-ch/\kappa}. \label{eq:single-shock-away-step2}\tag{224}\]
Therefore, by the triangle inequality, \[\|f^\kappa-M^{E,\kappa}\|_{L^2_\xi(M_\#^{-1})} \le \|f^\kappa-\bar f^\kappa\|_{L^2_\xi(M_\#^{-1})} + \|\bar f^\kappa-M^{E,\kappa}\|_{L^2_\xi(M_\#^{-1})}.\] Taking the supremum over \((\tau,y)\in\Omega^\kappa_{h,T}\), and using 223 and 224 , yields [eq:single-shock-away-modulated]. Since \(\mathcal{E}^\kappa(0)\to0\) and \(e^{-ch/\kappa}\to0\) for every fixed \(h>0\), the convergence statement follows. ◻
Remark 4. Assume in addition that \(X^\kappa(0)=0\). Since Proposition 8 yields \[\int_0^T \delta |\dot{X}^\kappa(\tau)|^2\,d\tau \le C\,\mathcal{E}_{\mathrm{sh}}^\kappa(0)^2,\] we have \[|X^\kappa(\tau)| = \left|\int_0^\tau \dot{X}^\kappa(s)\,ds\right| \le \tau^{1/2} \left(\int_0^\tau |\dot{X}^\kappa(s)|^2\,ds\right)^{1/2} \le T^{1/2}\delta^{-1/2} \left(\int_0^T \delta |\dot{X}^\kappa(\tau)|^2\,d\tau\right)^{1/2}.\] Hence \[\sup_{0\le\tau\le T}|X^\kappa(\tau)| \le C_T \mathcal{E}_{\mathrm{sh}}^\kappa(0)\to0 \qquad\text{as }\kappa\to0.\]
Therefore, for every fixed \(h>0\), if \(\kappa\) is sufficiently small so that \[\sup_{0\le\tau\le T}|X^\kappa(\tau)|\le \frac{h}{2},\] then \[|y-s\tau|\ge h \quad\Longrightarrow\quad |y-s\tau-X^\kappa(\tau)|\ge \frac{h}{2}.\] Applying Theorem 3 with \(h/2\) in place of \(h\), we conclude that the same convergence statement holds uniformly on the region \[\{(\tau,y)\in[0,T]\times\mathbb{R}:\;|y-s\tau|\ge h\},\] that is, away from the unmodulated Euler shock curve \(y=s\tau\).
We first recall the \(1\)-rarefaction wave for the compressible Euler system. Let \[(v^r,u^r,\theta^r)(t,x) = (v^r,u^r,\theta^r)\!\left(\frac{x}{t}\right)\] be the self-similar \(1\)-rarefaction wave fan solving \[v_t-u_{1x}=0,\qquad u_{1t}+p_x=0,\qquad u_{it}=0 \;\;(i=2,3),\qquad \left(\theta+\frac{|u|^2}{2}\right)_t+(pu_1)_x=0,\] with Riemann initial data \[(v,u,\theta)(0,x)= \begin{cases} (v_-,u_-,\theta_-), & x<0,\\ (v_*,u_*,\theta_*), & x>0, \end{cases}\] where \[u_-=(u_{1-},0,0),\qquad u_*=(u_{1*},0,0).\]
To construct a smooth approximate rarefaction wave for the Boltzmann equation, we introduce the smooth solution \(w^{R,\kappa}\) of the Burgers equation \[w^{R,\kappa}_t+w^{R,\kappa} w^{R,\kappa}_x=0, \qquad w^{R,\kappa}(0,x)=\frac{w_*+w_-}{2}+\frac{w_*-w_-}{2}\tanh \frac{x}{\kappa}.\] We then define the smooth approximate rarefaction wave \((v^{R,\kappa},u^{R,\kappa},\theta^{R,\kappa})(t,x)\) by \[\label{eq:rare1} \begin{align} &w_-=\lambda_{1-}:=\lambda_1(v_-,\theta_-), \quad w_*=\lambda_{1*}:=\lambda_1(v_*,\theta_*), \quad \lambda_1(v,\mathfrak s_*) := \lambda_1(v,\theta(v;\mathfrak s_*)),\\ &\lambda_1\bigl(v^{R,\kappa}(t,x),\theta^{R,\kappa}(t,x)\bigr)=w^{R,\kappa}(t+1,x),\\ &u_1^{R,\kappa}(t,x)=u_{1*}-\int_{v_*}^{v^{R,\kappa}(t,x)}\lambda_1(v,s_*)\,dv,\\ &\mathfrak s\bigl(v^{R,\kappa}(t,x),\theta^{R,\kappa}(t,x)\bigr)=\mathfrak s_*,\\ &u_i^{R,\kappa}(t,x)\equiv 0,\qquad i=2,3. \end{align}\tag{225}\] Here \(\lambda_1(v,s_*)\) denotes the first characteristic speed along the isentrope \(\mathfrak s=\mathfrak s_*\).
The construction of the smooth approximate rarefaction wave is standard in the Boltzmann–Euler setting; see [63], [64], [65] and [57]. Here, we record only the properties of the rarefaction wave that are used in our analysis. The remaining properties are mainly needed to derive the a priori estimate. For the a priori estimate related to the rarefaction-contact discontinuity-shock composite wave, we refer the reader to [38].
Lemma 43. Let \[\delta_R:=|v_*-v_-| \sim |u_{1*}-u_{1-}| \sim |\theta_*-\theta_-|\] denote the strength of the rarefaction wave. Then the smooth approximate \(1\)-rarefaction wave \((v^{R,\kappa},u_1^{R,\kappa},\theta^{R,\kappa})(t,x)\) defined in 225 satisfies the following properties.
For all \(x\in\mathbb{R}\) and \(t\ge0\), \[u_{1x}^{R,\kappa}=\frac{3v^{R,\kappa}}{4}w_x^{R,\kappa}>0, \qquad v_x^{R,\kappa}=\frac{3v^{R,\kappa}}{\sqrt{10\theta^{R,\kappa}}}u_{1x}^{R,\kappa}>0, \qquad \theta_x^{R,\kappa}=-\frac{2\theta^{R,\kappa}}{3v^R}v_x^{R,\kappa}<0.\]
For some \(\kappa_0>0\), such that \(\forall \kappa\in(0,\kappa_0]\), \(\forall p\in[1,+\infty]\) and \(\forall t>0\), \[\begin{align} \label{eq:rarmai} \bigl\lVert(v^{R,\kappa}-v^{r},u_1^{R,\kappa}-u^r,\theta^{R,\kappa}-\theta^r)(\cdot,t)\bigr\rVert_{L^p} \le C_p \delta_R \kappa^{1/p} \end{align}\qquad{(54)}\]
Proof. The proof is the same as that in [65]. ◻
Corollary 3 (Rarefaction–contact–shock case). Let \(U_+\), \(\kappa_0\), \(\delta_{\mathrm{res},0}\), \(\varepsilon_{\mathrm{res},0}\), and \(M_\#=M[U_\#]\) be as in Theorem 2. Let \(0<\delta\le \delta_{\mathrm{res},0}\), and let \[U^E=(v^E,u^E,\theta^E)(t,x)\] be a Riemann solution to the one-dimensional compressible Euler system 3 , connecting \[U_-:=(v_-,u_{1-},\theta_-) \qquad \text{to} \qquad U_+,\] through two intermediate states \(U_*\) and \(U^*\), with total wave strength \[\delta=\delta_R+\delta_C+\delta_S\] where \(\delta_R\), \(\delta_C\), and \(\delta_S\) the strengths of the rarefaction, contact, and shock components, respectively. Assume that \(U^E\) is a superposition of a \(1\)-rarefaction wave, a \(2\)-contact discontinuity, and a \(3\)-shock wave.
For each \(0<\varepsilon_1\le \varepsilon_{\mathrm{res},0}\) and \(0<\kappa\le \kappa_0\), let \(f_0^\kappa\) be a nonnegative smooth initial datum satisfying the well-preparedness condition 8 . Let \(f^\kappa\) be the corresponding solution to the Boltzmann equation 2 on a time interval \([0,T]\), where \(T>0\) is arbitrary.
Then \(f^\kappa\) exists uniquely on \([0,T]\). Moreover, there exist \[X_3^0\in BV([0,T])\] and a family of shifts \(\{X_3^\kappa\}_{\kappa>0}\) such that, up to extraction of a subsequence, \[X_3^\kappa \to X_3^0 \qquad \text{in } L^1(0,T) \qquad \text{as } \kappa\to0,\] and \[\begin{align} \label{eq:hlmt-main} &\int_0^T \iint_{\mathbb{R}\times\mathbb{R}^3} \left|f^\kappa-M_{X_3^0}[U^E]\right|^2 \,d\xi\,dy\,dt \nonumber\\ &\qquad \le C\kappa\bigl((\varepsilon_1+\delta_{\mathrm{res},0})^2+\delta_{\mathrm{res},0}^{1/2}\bigr)T + C(\delta_R+\delta_C)\kappa^{1/2}T^{3/2} + C\delta_{\mathrm{res},0}^2\|X_3^\kappa-X_3^0\|_{L^1(0,T)}. \end{align}\qquad{(55)}\] Here the positive constant \(C\) is independent of \(\kappa\) and \(T\).
In this case, since the 3-shock will be shifted only, for simplicity we work in the moving frame and use the normalized equation: \[\begin{align} \begin{aligned}\label{eq:Yibel} &f_t-\sigma f_z-\frac{u_1}{v}f_z+\frac{\xi_1}{v}f_z=\mathcal{N}(f,f)\\ &f(0,z,\xi)=f_0(z,\xi). \end{aligned} \end{align}\tag{226}\] We also need the following result.
Proposition 9. (see [38]) For each \((v_+,u_+,\theta_+)\) with \(v_+,\theta_+>0\), let \((v_-,u_-,\theta_-)\) satisfies that the Riemann problem of Euler equations 3 consists of a \(1\)-rarefaction wave, a \(2\)-contact discontinuity, and a \(3\)-shock wave. Suppose that \(f(t,y,\xi)\) is a solution to 226 on \(t\in[0,T]\). Then there exist positive constants \(C_0,\delta_{\mathrm{res},0},\varepsilon_{\mathrm{res},0}\) (\(\delta_{\mathrm{res},0},\varepsilon_{\mathrm{res},0}<1\)) and a global Maxwellian \(M_\#=M[U_\#](v_\#,\theta_\#>0)\) independent of time \(T\) such that if the wave strength \(\delta_R+\delta_C+\delta_S\leq \delta_{\mathrm{res},0}\) and \(\mathcal{E}(T)\leq \varepsilon\), then it holds that \[\begin{align} \begin{aligned} &\mathcal{E}(T)^2 + \delta_S\int_0^T \left| \dot{X}(t)\right|^2 dt + \int_0^T \left(\mathcal{G}^R+\mathcal{G}^S\right)dt + \sum_{\left| \beta\right|=1}\int_0^T \bigl\lVert\partial^\beta(\phi,\psi,\zeta)\bigr\rVert_{L^2}^2dt\\ &+\int_0^T\left(\bigl\lVert(\phi_{zz},\psi_{zz},\zeta_{zz})\bigr\rVert_{L^2}^2+\bigl\lVert(\phi_{zt},\psi_{zt},\zeta_{zt})\bigr\rVert_{L^2}^2\right) dt \\ &+\int_0^T \int \bigl\lVert\widetilde{G}_{\mathrm{rem}}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_z\bigr\rVert_{\nu,M_\#}^2 +\bigl\lVert\widetilde{G}_t\bigr\rVert_{\nu,M_\#}^2 +\bigl\lVert\widetilde{G}_{zz}\bigr\rVert_{\nu,M_\#}^2 + \bigl\lVert\widetilde{G}_{zt}\bigr\rVert_{\nu,M_\#}^2 dz dt\\ &\leq C_0\left(\mathcal{E}(0)^2+\delta_{\mathrm{res},0}^{1/2}\right), \end{aligned} \end{align}\] where \(\partial^\beta=\partial_t^{\beta_0}\partial_z^{\beta_1}\), \(|\beta|=|\beta_1|+|\beta_0|\) denotes the derivatives with respect to \(z\) or \(t\), and \[\begin{align} \begin{aligned} & \mathcal{G}^R:=\int\left| v^R_z\right|\left| (\phi,\zeta)\right|^2 dy,\\ & \mathcal{G}^S:=\int\Bigl|\partial_z\left(v^{S_3}\right)^{-X_3}\Bigr|\left| \left(\phi,\psi,\zeta\right)\right|^2 dy. \end{aligned} \end{align}\]
Proof of Corollary 3. By Proposition 9, together with the same local existence and continuation argument used in the proof of Theorem 2, there exists a unique global normalized solution in the moving frame, together with a shift \(X_3=X_3(t)\).
Let \(f\) denote this normalized solution, and define the rescaled physical solution and shift by 51 and 52 . Equivalently, \[f^\kappa(\tau,y,\xi)=f\!\left(\frac{\tau}{\kappa},\frac{y}{\kappa},\xi\right), \qquad X_3^\kappa(\tau)=\kappa X_3\!\left(\frac{\tau}{\kappa}\right).\] Then \(f^\kappa\) exists uniquely on \([0,T]\) for every \(T>0\), since \(f\) exists globally on \([0,\infty)\).
We first compare \(f^\kappa\) with the rescaled composite approximate wave \(\bar f^{\,\kappa}\). By Proposition 9, after the same scaling argument as in the proof of Theorem 2, we obtain the perturbation estimate \[\begin{align} \int_0^T\int_{\mathbb{R}} \bigl\lVert f^\kappa-\bar f^{\kappa}\bigr\rVert_{M_\#}^2 \,dy\,d\tau \le C\kappa\bigl((\varepsilon_1+\delta_{\mathrm{res},0})^2+\delta_{\mathrm{res},0}^{1/2}\bigr)T . \label{eq:main-step-1-rare-cor} \end{align}\tag{227}\]
Next we prove compactness of the rescaled shift family. By 52 , \[\frac{d}{d\tau}X_3^\kappa(\tau) = \dot{X}_3\!\left(\frac{\tau}{\kappa}\right)\] for a.e. \(\tau\in(0,T)\), and therefore \[\operatorname{TV}(X_3^\kappa;[0,T]) = \int_0^T \left|\frac{d}{d\tau}X_3^\kappa(\tau)\right|\,d\tau = \kappa \int_0^{T/\kappa} |\dot{X}_3(t)|\,dt.\] By Cauchy–Schwarz and Proposition 9, \[\operatorname{TV}(X_3^\kappa;[0,T]) \le \kappa^{1/2}T^{1/2} \left(\int_0^{T/\kappa} |\dot{X}_3(t)|^2\,dt\right)^{1/2} \le C_T \delta_S^{-1/2}.\] Hence \(\{X_3^\kappa\}_{\kappa>0}\) is uniformly bounded in \(BV(0,T)\), and thus, after extraction of a subsequence if necessary, there exists \(X_3^0\in BV([0,T])\) such that \[X_3^\kappa \to X_3^0 \qquad\text{in }L^1(0,T).\]
We now compare the rescaled composite wave with the shifted Euler Maxwellian profile. Combining the smooth rarefaction approximation estimate from Lemma 43 with the corresponding contact-wave estimate, we obtain \[\begin{align} \int_0^T\int_{\mathbb{R}} \bigl\lVert\bar f^{\,\kappa}-M_{X_3^\kappa}[U^E]\bigr\rVert_{M_\#}^2\,dy\,d\tau \le C(\delta_R+\delta_C)\kappa^{1/2}T^{3/2}+C\delta_S\kappa T . \label{eq:main-step-2-rare-cor} \end{align}\tag{228}\]
Finally, by the mean value theorem and the exponential decay of the Euler shock profile, for each \(\tau\in[0,T]\), \[\begin{align} \int_{\mathbb{R}} \bigl\lVert M_{X_3^\kappa}[U^E]-M_{X_3^0}[U^E]\bigr\rVert_{M_\#}^2 \,dy \le C\delta_{\mathrm{res},0}^2|X_3^\kappa(\tau)-X_3^0(\tau)|. \end{align}\] Integrating in \(\tau\) yields \[\begin{align} \int_0^T\int_{\mathbb{R}} \bigl\lVert M_{X_3^\kappa}[U^E]-M_{X_3^0}[U^E]\bigr\rVert_{M_\#}^2 \,dy\,d\tau \le C\delta_{\mathrm{res},0}^2\|X_3^\kappa-X_3^0\|_{L^1(0,T)}. \label{eq:main-step-3-rare-cor} \end{align}\tag{229}\]
Combining 227 , 228 , and 229 , and using that \(M_\#\) is uniformly bounded from above and below by positive constants, we conclude that \[\begin{align} &\int_0^T \int_{\mathbb{R}} \bigl\lVert f^\kappa-M_{X_3^0}[U^E]\bigr\rVert_{M_\#}^2 \,dy\,d\tau\\ &\qquad \le C\kappa\bigl((\varepsilon_1+\delta_{\mathrm{res},0})^2+\delta_{\mathrm{res},0}^{1/2}\bigr)T + C(\delta_R+\delta_C)\kappa^{1/2}T^{3/2} + C\delta_{\mathrm{res},0}^2\|X_3^\kappa-X_3^0\|_{L^1(0,T)}. \end{align}\] This is exactly ?? . ◻
CK is partially supported by NSF-CAREER 2047681. This material is partly based upon work supported by the National Science Foundation under Grant No. DMS-2424139, while one of the authors (C.K.) was in residence at the Simons Laufer Mathematical Sciences Institute in Berkeley, California, during the Fall 2025 semester.
In this appendix, we collect several standard estimates for the hard-sphere collision operator that will be used repeatedly in the main text. We refer to [58], [66] for the basic macro–micro framework and weighted estimates.
We first recall the decomposition of the collision operator into the gain and loss parts: \[\label{eq:Q-gain-loss} \mathcal{N}(g,h)=\mathcal{N}^+(g,h)-\mathcal{N}^-(g,h).\tag{230}\]
The following weighted \(L^2\) estimates are standard for the hard-sphere collision operator.
Lemma 44. There exists a positive constant \(C\) such that \[\begin{align} \int_{\mathbb{R}^3}\frac{(1+|\xi|)^{-1}|\mathcal{N}^-(g,h)|^2}{M_\#}\,d\xi &\le C \bigl\lVert g\bigr\rVert_{\nu,M_\#}^2\, \bigl\lVert h\bigr\rVert_{M_\#}^2, \label{eq:collision-loss} \\ \int_{\mathbb{R}^3}\frac{(1+|\xi|)^{-1}|\mathcal{N}_+(g,h)|^2}{M_\#}\,d\xi &\le C \bigl\lVert g\bigr\rVert_{M_\#}^2 \, \bigl\lVert h\bigr\rVert_{\nu,M_\#}^2 \label{eq:collision-gain} \end{align}\] {#eq: sublabel=eq:eq:collision-loss,eq:eq:collision-gain} Consequently, \[\begin{align} &\int_{\mathbb{R}^3}\frac{(1+|\xi|)^{-1}|\mathcal{N}(g,h)|^2}{M_\#}\,d\xi\nonumber \\ &\quad \le C\Bigl[ \bigl\lVert g\bigr\rVert_{\nu,M_\#}^2\, \bigl\lVert h\bigr\rVert_{M_\#}^2 + \bigl\lVert g\bigr\rVert_{M_\#}^2 \, \bigl\lVert h\bigr\rVert_{\nu,M_\#}^2 \Bigr]. \label{eq:collision-Q} \end{align}\qquad{(56)}\] Here \(M_\#\) is a reference global Maxwellian and the above estimates hold on a uniform class of functions comparable to \(M_\#\).
Let \(M=M[U]\) where \(U=(v,u,\theta)\) be a local Maxwellian and let \(L_M\) denote the linearized collision operator around \(M\). Let \(\mathfrak Z_M\) be the null space of \(L_M\), and let \(\mathfrak Z_M^\perp\) be its orthogonal complement.
Lemma 45. Let \(U_\#=(v_\#,u_\#,\theta_\#)\), \(M_\#:=M[U_\#]\). Then there exists a constant \(\eta_0>0\) such that the following holds. Let \(\mathcal{K}_\#\Subset \mathbb{R}_{>0}\times \mathbb{R}^3\times \mathbb{R}_{>0}\) be a compact set satisfying \[\mathcal{K}_\# \subset B_{\eta_0}(U_\#),\qquad \theta_\#<\inf_{U\in\mathcal{K}_\#}\theta \le \sup_{U\in\mathcal{K}_\#}\theta<2\theta_\#\] where \(B_{\eta_0}(U_\#):=\{U\in\mathbb{R}_{>0}\times\mathbb{R}^3\times \mathbb{R}_{>0}:|U-U_\#|<\eta_0\}\). For \(U=(v,u,\theta)\in\mathcal{K}_\#\), set \(M=M[U]\). Then there exists a constant \(\lambda_{\mathrm{mic}}>0\), depend only on \(\mathcal{K}_\#\) and \(U_\#\), such that \[\begin{align} \label{eq:collision-coercivity} -\int_{\mathbb{R}^3}\frac{gL_Mg}{M_\#}\,d\xi \ge \lambda_{\mathrm{mic}}\int_{\mathbb{R}^3}\frac{(1+|\xi|)g^2}{M_\#} \, d\xi \end{align}\qquad{(57)}\] for every \(U \in \mathcal{K}_\#\) and every \(g\in\mathfrak Z_M^\perp\). Moreover, \[\begin{align} \label{eq:collision-inverse} \int_{\mathbb{R}^3}\frac{(1+|\xi|)}{M_\#}|L_M^{-1}g|^2 \, d\xi \le \lambda_{\mathrm{mic}}^{-2} \int_{\mathbb{R}^3}\frac{(1+|\xi|)^{-1}g^2}{M_\#}\, d\xi \end{align}\qquad{(58)}\] Here \(\mathfrak Z_M\) is the null-space of \(L_M\).
We now record two elementary lemmas needed to pass from the a priori estimate to the pointwise-in-space control of the perturbation.
Lemma 46 (One-dimensional Sobolev embedding with values in a Hilbert space). Let \(H\) be a Hilbert space. Then for every \(g\in H^1(\mathbb{R}_y;H)\), \[\sup_{y\in\mathbb{R}}\|g(y)\|_H^2 \le 2\|g\|_{L^2_y(H)}\|g_y\|_{L^2_y(H)} \le \|g\|_{H^1_y(H)}^2 . \label{eq:H1-Linfty-Hilbert-single}\qquad{(59)}\] In particular, \[H^1(\mathbb{R}_y;H)\hookrightarrow C_b^0(\mathbb{R}_y;H).\]
Proof. It is enough to prove ?? for \(g\in C_c^\infty(\mathbb{R}_y;H)\), the general case following by density. For such \(g\), \[\frac{d}{dy}\|g(y)\|_H^2 = 2\langle g_y(y),g(y)\rangle_H .\] Hence, for every \(y\in\mathbb{R}\), \[\|g(y)\|_H^2 = 2\int_{-\infty}^y \langle g_z(z),g(z)\rangle_H\,dz \le 2\int_{\mathbb{R}}\|g_z(z)\|_H\,\|g(z)\|_H\,dz .\] By Cauchy–Schwarz, \[\|g(y)\|_H^2 \le 2\|g_y\|_{L^2_y(H)}\|g\|_{L^2_y(H)} .\] Taking the supremum in \(y\) proves ?? . ◻
Lemma 47 (Local Lipschitz continuity of the Maxwellian map). Let \(K\Subset \mathbb{R}_+\times\mathbb{R}\times\mathbb{R}_+\) be compact. Then there exists \(C_K>0\) such that \[\|M[U]-M[V]\|_{M_\#} \le C_K |U-V|, \qquad U,V\in K. \label{eq:Maxwellian-Lipschitz-single}\qquad{(60)}\]
Proof. Let \(U,V\in K\), and define \(U_\vartheta:=(1-\vartheta)V+\vartheta U\), \(\vartheta\in[0,1]\). Enlarging \(K\) slightly if necessary, we may assume that the whole segment \(\{U_\vartheta:\vartheta\in[0,1]\}\) lies in a compact set \(K'\Subset \mathbb{R}_+\times\mathbb{R}\times\mathbb{R}_+\). By the fundamental theorem of calculus, \[M[U]-M[V] = \int_0^1 DM[U_\vartheta](U-V)\,d\vartheta .\] Hence \[\|M[U]-M[V]\|_{M_\#} \le |U-V| \sup_{W\in K'} \|DM[W]\|_{\mathcal{L}(\mathbb{R}^3,L^2_\xi(M_\#))}.\] It therefore suffices to bound \(DM[W]\) uniformly on \(K'\). Each partial derivative \(\partial_{W_j}M[W]\) is of the form \(P_j(\xi;W)M[W](\xi)\), where \(P_j\) is a polynomial of degree at most \(2\) in \(\xi\), with coefficients depending continuously on \(W\). Since \(K'\) is compact and bounded away from vacuum and zero temperature, there exist positive constants \(C,c\) such that \[\frac{M[W](\xi)^2}{M_\#(\xi)} \le Ce^{-c|\xi|^2}, \qquad W\in K',\;\xi\in\mathbb{R}^3.\] Therefore \[\sup_{W\in K'} \sum_j \|\partial_{W_j}M[W]\|_{M_\#} <\infty,\] which implies ?? . ◻
Proof. We do not reproduce the proof of the corresponding estimates for \(3\)-shock wave here, since it is essentially the same as the proof given in [38]. In particular, the estimates for the \(3\)-shock profile will be used in the form established in [20]. Our purpose in the above discussion is only to make explicit the scalar parametrization and the auxiliary estimates from [38], which are invoked in the proof of [20]. We first recall the scalr parametrization of a Boltzmann shock profile. By (295) in [20], there exists a scalar function \(\eta=\eta(y)\) such that \[\label{eq:scalar-param-zeta} \left\{ \begin{align} \eta_y &= a_0(\eta)\bigl(\eta-\eta_-\bigr)\bigl(\eta-\eta_+\bigr), \\ \eta(-\infty) &= \eta_-, \qquad \eta(+\infty) = \eta_+, \end{align} \right.\tag{231}\] where \(\eta_->0>\eta_+\), \(|\eta_- - \eta_+| = O(\delta_3)\), and \(a_0\) is a smooth function satisfying \(a_0(\eta)\ge c>0\). The elementary consequences of 231 , including the monotonicity, exponential decay, the higher derivative estimates of \(\eta\), are obtained in [20]. In particular, we shall use \[\label{eq:zeta-basic-estimates} \eta_y<0, \qquad |\eta-\eta_\pm| \lesssim \delta_3 e^{-c \delta_3 |y|} \quad \text{as } y\to \pm \infty,\tag{232}\] and \[\label{eq:zeta-derivative-estimates} |\eta_y| \lesssim \delta_3^2 e^{-c\delta_3 |y|}, \qquad |\partial_y^k \eta| \lesssim \delta_3^{k-1}|\eta_y|, \qquad k\ge 2.\tag{233}\] by (295) in [20] and Lemma A.1 in [38]. Under this parametrization, the macroscopic part of the shock profile satisfies \[\label{eq:macro-zeta-comparison} \bigl|v_y^{S_3}\bigr| \sim \bigl|u_{1y}^{S_3}\bigr| \sim \bigl| \theta_y^{S_3}\bigr| \sim |\eta_y|.\tag{234}\] Moreover, by (289) and (291) in [20], the microscopic component can be represented in the form \[G^{S_3}(y,\xi) = \sqrt{M_\#} \, \Gamma(\chi(\eta(y)),\xi),\] where \(M_\#\) is a fixed global Maxwellian, \(\Gamma\) is smooth and \(\chi=\chi(\eta)\) is determined by \[\label{eq:chi-equation} \chi(\eta) = b(\eta,\chi(\eta)) (\eta- \eta_-) (\eta-\eta_+),\tag{235}\] where \(b\) is smooth and uniformly bounded above and below by postivie constants. Consequently, \[\label{eq:G-chi-relation} \Bigl( \int_{\mathbb{R}^3} \frac{(1+|\xi|)\bigl|G^{S_3}(y,\xi)\bigr|^2}{M_\#}\, d\xi \Bigr)^{\frac{1}{2}} = |\chi(\eta(y))|\, c_0 (\chi(\eta(y))),\tag{236}\] where \(c_0\) is smooth and satisfies \(c_0\ge c>0\).
By referring to [38], we obtain the corresponding estimate for the \(3\)-shock. We prove the \(1\)-shock estimate by using the reflection symmetry from the corresponding \(3\)-shock estimate. Let \[\begin{align} U^{S_1} = (v^{S_1},u^{S_1},\theta^{S_1}) \end{align}\] be the \(1\)-shock profile connecting \(U_-=(v_-,u_-,\theta_-)\) to \(U_*=(v_*,u_*,\theta_*)\). Define the reflected profiles by \[\begin{align} \widetilde{v}^{S_3}(z) := v^{S_1}(-z), \quad \widetilde{u}^{S_3}(z) := -u^{S_1}(-z), \quad \widetilde{\theta}^{S_3}(z) := \theta^{S_1}(-z). \end{align}\] Then \(\widetilde{U}^{S_3}\) is a \(3\)-shock profile connecting \(\widetilde{U}^*=(v_*,-u_*,\theta_*)\) to \(\widetilde{U}_+=(v_-,-u_-,\theta_-)\). In particular, we denote \(\widetilde{v}^*=v_*\), \(\widetilde{v}_+=v_-\), \(\widetilde{\theta}^*= \theta_*\), \(\widetilde{p}^*=p_*\) and \(\widetilde{p}_+=p_-\). Note that \(\widetilde{p}^{S_3}(z) = p^{S_1}(-z)\) since \(p=p(v,\theta)\). Moreover the shock strength is preserved under reflection, namely, \(\widetilde{\delta}_3=\delta_1\). Applying the \(3\)-shock estimate to the reflected profile gives \[\begin{align} &\Biggl|\frac{\widetilde{p}^{S_3}-\widetilde{p}_+}{\widetilde{v}^{S_3}-\widetilde{v}_+}- \frac{\widetilde{p}^{S_3}-\widetilde{p}^*}{\widetilde{v}^{S_3}-\widetilde{v}^*}-\frac{5\widetilde{p}^*}{9\bigl(\widetilde{v}^*\bigr)^2}\Bigl(\frac{10\mu(\widetilde{\theta}^*)-9\alpha_{\rm th}(\widetilde{\theta}^*)}{10\mu(\widetilde{\theta}^*)+3\alpha_{\rm th}(\widetilde{\theta}^*)}+3\Bigr)\Biggr| \le C\widetilde{\delta}_3^2. \end{align}\] Using the above identifications, this becomes \[\begin{align} &\Biggl|\frac{p^{S_1}-p_-}{v^{S_1}-v_-}- \frac{p^{S_1}-p_*}{v^{S_1}-v_*}-\frac{5p_*}{9\bigl(v_*\bigr)^2}\Bigl(\frac{10\mu(\theta_*)-9\alpha_{\rm th}(\theta_*)}{10\mu(\theta_*)+3\alpha_{\rm th}(\theta_*)}+3\Bigr)\Biggr| \le C\delta_1^2. \end{align}\] This proves the desired \(1\)-shock estimate. The remaining estimates for \(1\)-shock can be derived in a similar manner. ◻
Proof. The proof follows a similar argument to that in [34]. We provide the details for completeness. Let \[x_1(t):=\sigma_1 t+X_1(t), \qquad x_3(t):=\sigma_3 t+X_3(t).\] By the exponential localization of each viscous shock profile, there exist positive constants \(c\) and \(C\) such that \[\label{eq:shock-tail-proof} \bigl|\partial_x(v^{S_i})^{-X_i}(t,x)\bigr| \le C\delta_i^2 e^{-c\delta_i|x-x_i(t)|}, \qquad i=1,3.\tag{237}\] Moreover, in the present \(1\)-shock/\(3\)-shock configuration, the two shifted shock locations remain separated linearly in time. More precisely, after possibly decreasing \(\delta_0>0\), we may assume that there exists a constant \(c_1,c_3>0\) such that \[\label{eq:shock-separation-proof} x_1(t)\le -c_1 t, \qquad x_3(t)\ge c_3 t, \qquad t>0.\tag{238}\]
We first prove the estimate for \(\varphi_3 |(v^{S_1})_x^{-X_1}|\). By the definition of \(\varphi_1\) and \(\varphi_3\), if \(\varphi_3(t,x)\neq0\), then \[x\ge \frac{x_1(t)}{2}.\] Since \(x_1(t)<0\) by 238 , it follows that \[x-x_1(t) \ge -\frac{x_1(t)}{2} \ge \frac{c_1}{2}\,t>0.\] Hence, by 237 , \[\varphi_3(t,x)\bigl|\partial_x(v^{S_1})^{-X_1}(t,x)\bigr| \le C\delta_1^2 e^{-c\delta_1|x-x_1(t)|} \le C\delta_1^2 e^{-C\delta_1 t}.\] This proves the first estimate in ?? .
Similarly, if \(\varphi_1(t,x)\neq0\), then \[x\le \frac{x_3(t)}{2}.\] Since \(x_3(t)>0\) by 238 , we obtain \[x_3(t)-x \ge \frac{x_3(t)}{2} \ge \frac{c_3}{2}\,t>0.\] Using again 237 , we get \[\varphi_1(t,x)\bigl|\partial_x(v^{S_3})^{-X_3}(t,x)\bigr| \le C\delta_3^2 e^{-C\delta_3 t},\] which proves the second pointwise estimate.
We next prove the integral estimates. By the pointwise bound just proved, \[\int_{\mathbb{R}}\varphi_3(t,x)\bigl|\partial_x(v^{S_1})^{-X_1}(t,x)\bigr|\,dx \le C\delta_1^2 \int_{\{x\ge x_1(t)/2\}} e^{-c\delta_1|x-x_1(t)|}\,dx.\] Since \(x\ge x_1(t)/2\) implies \(|x-x_1(t)|\ge |x_1(t)|/2\ge c_1 t/2\), we have \[\int_{\{x\ge x_1(t)/2\}} e^{-c\delta_1|x-x_1(t)|}\,dx \le C\int_{c_1 t/2}^{\infty} e^{-c\delta_1 z}\,dz \le C\delta_1^{-1}e^{-C\delta_1 t}.\] Therefore, \[\int_{\mathbb{R}}\varphi_3(t,x)\bigl|\partial_x(v^{S_1})^{-X_1}(t,x)\bigr|\,dx \le C\delta_1 e^{-C\delta_1 t}.\] The estimate \[\int_{\mathbb{R}}\varphi_1(t,x)\bigl|\partial_x(v^{S_3})^{-X_3}(t,x)\bigr|\,dx \le C\delta_3 e^{-C\delta_3 t}\] is proved in the same way.
This completes the proof. ◻
Proof. The proof follows a similar argument to that in [37]. We provide the details for completeness. We only prove ?? and ?? , since ?? –?? follow in exactly the same way.
Set \[\xi_1(t):=\sigma_1 t+X_1(t), \qquad \xi_3(t):=\sigma_3 t+X_3(t).\] By the standard pointwise estimates for the viscous shock profiles and the viscous contact wave obtained earlier, we have \[\begin{align} \tag{239} |\partial_x(v^{S_1})^{-X_1}(t,x)| &\le C\delta_1^2 e^{-c\delta_1|x-\xi_1(t)|}, \quad x-\xi_1(t)\in \mathbb{R} \\ \tag{240} |(v^{S_3}-v^*,\theta^{S_3}-\theta^*)^{-X_3}(t,x)| &\le C\delta_3 e^{-c\delta_3|x-\xi_3(t)|}, \quad x-\xi_3(t)\leq0, \\ \tag{241} |(v^C-v_*,\theta^C-\theta_*)(t,x)| &\le C\delta_C(1+t)^{-1/2}e^{-c_0x^2/(1+t)}, \quad x\leq 0. \end{align}\] Moreover, since the shock speeds are distinct and the shifts are bounded in the regime of interest, there exists a positive constant \(c_1\) such that \[\label{eq:proof-int-sep} |\xi_3(t)-\xi_1(t)|\ge c_1(1+t), \qquad |\xi_1(t)|+|\xi_3(t)|\ge c_1(1+t).\tag{242}\]
We first prove ?? . We divide into two regions \(A_1:=\{x-\sigma_1t\geq -\frac{\sigma_1}{2}t\}\) and \(A_2:=\mathbb{R}-A_1\). Since \[\begin{align} & x-\xi_1(t) \geq -\frac{\sigma_1}{2}t + C\varepsilon t\geq -\frac{\sigma_1t}{4}>0 \quad \text{for}\, x\in A_1,\\ & x\leq \frac{\sigma_1}{2}t <0,\quad \text{for} \, x\in A_2, \end{align}\] we have the following observations. \[\begin{align} \label{eq:keysep1} \left| \partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|\leq C \delta_1^2 e^{-C\delta_1\left| x-\xi_1(t)\right|} \leq C \delta_1^2 e^{-\frac{C\delta_1}{2}\left| x-\xi_1(t)\right|}e^{-C\delta_1t}. \end{align}\tag{243}\]
By 239 , 241 and 243 , \[\begin{align} &\left\| |\partial_x(v^{S_1})^{-X_1}| \,|(v^C-v_*,\theta^C-\theta_*)| \right\|_{L^2_x}^2 \\ &\le \int_{A_1}|\partial_x(v^{S_1})^{-X_1}|^2 \,|(v^C-v_*,\theta^C-\theta_*)|^2 dx + \int_{A_2}|\partial_x(v^{S_1})^{-X_1}|^2 \,|(v^C-v_*,\theta^C-\theta_*)|^2 dx\\ &\le C\delta_C^2 \int_{A_1} \delta_1^4 e^{-2c\delta_1\left| x-\xi_1(t)\right|} dx + \frac{C}{1+t}\int_{A_2} \delta_1^4\delta_C^2 e^{-2c\delta_1\left| x-\xi_1(t)\right|}e^{-2c_0x^2/(1+t)} dx \\ &\le C\delta_C^2 \delta_1^3 e^{-C\delta_1t} + C\delta_C^2\delta_1^3e^{-Ct} \end{align}\] Therefore \[\left\| |\partial_x(v^{S_1})^{-X_1}| \,|(v^C-v_*,\theta^C-\theta_*)| \right\|_{L^2_x}^2 \le C\delta_1^3\delta_C^2 e^{-c\delta_1 t},\] which gives ?? .
Next, we prove ?? . Separate \(\mathbb{R}\) into \[\Omega_1 := \{x:x-\sigma_3t\leq -\frac{\sigma_3t}{2}\}, \qquad \Omega_2 := \mathbb{R}\setminus \Omega_1.\] Since \[\begin{align} &x-\xi_3(t)=x-\sigma_3t-X_3(t)\leq -\frac{\sigma_3t}{2}+C\varepsilon t\leq -\frac{\sigma_3t}{4}<0 \quad \text{for}\, x\in \Omega_1,\\ &x-\xi_1(t)=x-\sigma_1t-X_1(t)\geq \frac{\sigma_3t}{2}-\sigma_1t-C\varepsilon t\geq \frac{\sigma_3 t}{4}>0 \quad \text{for}\, x\in \Omega_2, \end{align}\] we have the following estimate. \[\begin{align} &\bigl\lVert\left| \partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|\left| \left(\bigl(v^{S_{3}}\bigr)^{-X_{3}}-v^*,\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}-\theta^*\right)\right|\bigr\rVert^2\\ &\le \int_{\Omega_1}\left| \partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|^2\left| \left(\bigl(v^{S_{3}}\bigr)^{-X_{3}}-v^*,\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}-\theta^*\right)\right|^2 dx\\ &\qquad+ \int_{\Omega_2} \left| \partial_x\bigl(v^{S_{1}}\bigr)^{-X_{1}}\right|^2\left| \left(\bigl(v^{S_{3}}\bigr)^{-X_{3}}-v^*,\bigl(\theta^{S_{3}}\bigr)^{-X_{3}}-\theta^*\right)\right|^2 dx \\ &\le C\delta_1^4\delta_3^2\int_{\Omega_1} e^{-2c\delta_1\left| x-\xi_1(t)\right|}e^{-2c\delta_3\left| x-\xi_3(t)\right|} dx + C\delta_1^4\delta_3^2\int_{\Omega_2} e^{-2c\delta_1\left| x-\xi_1(t)\right|} dx \\ &\le C\delta_1^3\delta_3^2e^{-c\delta_3t}+C\delta_1^3\delta_3^2e^{-c\delta_1t} \end{align}\] Thus \[\left\| |\partial_x(v^{S_1})^{-X_1}| \,|(v^{S_3}-v^*,\theta^{S_3}-\theta^*)^{-X_3}| \right\|_{L^2_x}^2 \le C\delta_1^3\delta_3^2 \bigl(e^{-c\delta_3 t}+e^{-c\delta_1 t}\bigr),\] and after taking square roots, \[\left\| |\partial_x(v^{S_1})^{-X_1}| \,|(v^{S_3}-v^*,\theta^{S_3}-\theta^*)^{-X_3}| \right\|_{L^2_x} \le C\delta_1^{3/2}\delta_3 \bigl(e^{-c\delta_3 t}+e^{-c\delta_1 t}\bigr).\] This proves ?? . ◻
Proof. The solutions are satisfied the following equations: \[\begin{align} \begin{aligned} &v_t-u_{1x}=0\\ &u_{1t}+p_x=-\int \xi_1^2 G_x d\xi\\ &u_{it}=-\int \xi_1\xi_i G_x d\xi,\quad (i=2,3)\\ &\theta_t+pu_{1x}=u_1\int \xi_1^2 G_x d\xi+\sum_{i=2}^3 u_i \int \xi_1\xi_i G_x d\xi-\frac{1}{2}\int \xi_1\left| \xi\right|^2 G_x d\xi. \end{aligned} \end{align}\]
For the approxiate solutions, we have the following systems: \[\begin{align} \begin{aligned} &v_t^C-u_{1x}^C=0\\ &u_{1t}^C+p_x^C=\frac{4}{3}\left(\frac{\mu\left(\theta^C\right)u_{1x}^C}{v^C}\right)_x+Q_1^C\\ &u_i^C = 0\quad (i=2,3)\\ &\theta_t^C + p^Cu_{1x}^C = \left(\frac{\alpha_{\rm{th}}\left(\theta^C\right)\theta_x^C}{v^C}\right)_x+\frac{4}{3}\mu\left(\theta^C\right)\frac{\left(u_{1x}^C\right)^2}{v^C}+Q_2^C \end{aligned} \end{align}\]
and
\[\begin{align} \begin{aligned} &\bigl((v^{S_{i}})^{-X_{i}}\bigr)_t+\dot{X}_i\bigl((v^{S_{i}})^{-X_{i}}\bigr)_x-\bigl((u_1^{S_{i}})^{-X_{i}}\bigr)_x=0\\ &\bigl((u_1^{S_{i}})^{-X_{i}}\bigr)_t+\dot{X}_i\bigl((u_1^{S_{i}})^{-X_{i}}\bigr)_x+\bigl((p^{S_{i}})^{-X_{i}}\bigr)_x=-\int\xi_1^2 \bigl((G^{S_{i}})^{-X_{i}}\bigr)_x d\xi\\ &\bigl(u_j^{S_{i}}\bigr)^{-X_{i}}\equiv 0 \quad(j=2,3)\\ &\bigl((\theta^{S_{i}})^{-X_{i}}\bigr)_t+\dot{X}_i\bigl((\theta^{S_{i}})^{-X_{i}}\bigr)_x+\bigl(p^{S_{i}}\bigr)^{-X_{i}}\bigl((u_1^{S_{i}})^{-X_{i}}\bigr)_x\\ &\qquad =\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\int \xi_1^2 \bigl((G^{S_{i}})^{-X_{i}}\bigr)_x d\xi -\frac{1}{2}\int \xi_1\left| \xi\right|^2 \bigl((G^{S_{i}})^{-X_{i}}\bigr)_xd\xi. \end{aligned} \end{align}\] Therefore, the perturbed systems are written by the micro part \(\widetilde{G}\):
\[\begin{align} \begin{aligned} &\phi_t-\psi_{1x}-\sum_{i=1,3} \dot{X}_i \bigl((v^{S_{i}})^{-X_{i}}\bigr)_x = 0\\ &\psi_{1t} + \left(p-p^{S_{1},-X_{1}}-p^C-p^{S_{3},-X_{3}}\right)_x-\sum_{i=1,3} \dot{X}_i \bigl((u_1^{S_{i}})^{-X_{i}}\bigr)_x \\ & \qquad = -Q_1^C-\frac{4}{3}\left(\frac{\mu\left(\theta^C\right)u_{1x}^C}{v^C}\right)_x-\int \xi_1^2 \widetilde{G}_x d\xi\\ &\psi_{it}=-\int \xi_1\xi_i \widetilde{G}_x d\xi,\quad (i=2,3)\\ &\zeta_t +\left(pu_{1x}-p^{S_{1},-X_{1}}\bigl((u_1^{S_{1}})^{-X_{1}}\bigr)_x-p^Cu_{1x}^C-p^{S_{3},-X_{3}}\bigl((u_1^{S_{3}})^{-X_{3}}\bigr)_x\right)-\sum_{i=1,3}\dot{X}_i\bigl((\theta^{S_{i}})^{-X_{i}}\bigr)_x\\ &\qquad \qquad = -\frac{1}{2}\int \xi_1 \left| \xi\right|^2 \widetilde{G}_x d\xi +u_1\int \xi_1^2 \widetilde{G}_x d\xi \\ &\qquad \qquad +\sum_{i=1,3} \left(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right)\int \xi_1^2 \bigl((G^{S_{i}})^{-X_{i}}\bigr)_x d\xi+\sum_{j=2}^3 u_j \int \xi_1\xi_j \widetilde{G}_x d\xi\\ &\qquad \qquad -\left(\frac{\alpha_{\rm{th}}\left(\theta^C\right)\theta_x^C}{v^C}\right)_x-\frac{4}{3}\mu\left(\theta^C\right)\frac{\left(u_{1x}^C\right)^2}{v^C}-Q_2^C. \end{aligned} \end{align}\]
We can easily get the following estimate for \(\phi_t\).
\[\begin{align} \begin{aligned} \bigl\lVert\phi_t\bigr\rVert_{L^2}^2 \leq C \int \left| \psi_{1x}\right|^2 dx + C\sum_{i=1,3} \left| \dot{X}_i\right|^2 \delta_i^2 \int \left| \bigl((v^{S_{i}})^{-X_{i}}\bigr)_x\right| dx \leq C \int \left| \psi_{1x}\right|^2 dx + C\sum_{i=1,3} \delta_i^3 \left| \dot{X}_i\right|^2 \end{aligned} \end{align}\]
For the estimate \(\psi_{1t}\), observe that \[\begin{align} \begin{aligned} \left(p-\overline{p}\right)_x =& \left(\frac{\zeta}{v}-\frac{\overline{\theta}\phi}{v\overline{v}}\right)_x \\ \leq & C \left| \left(\zeta_x,\zeta\overline{v}_x,\zeta\phi_x,\phi_x,\overline{\theta}_x\phi,\overline{v}_x\phi,\phi_x\phi\right)\right|\\ \leq & C\left| \left(\zeta_x,\phi_x\right)\right|+C\left| \left(\overline{\theta}_x,\overline{v}_x\right)\right|\left| \left(\zeta,\phi\right)\right|. \end{aligned} \end{align}\] By using this, we can compute as belowed: \[\begin{align} \begin{aligned} & \int \psi_{1t}\left(p-p^{S_{1},-X_{1}}-p^C-p^{S_{3},-X_{3}}\right)_x dx \\ & \quad \leq \frac{1}{64}\bigl\lVert\psi_{1t}\bigr\rVert_{L^2}^2 + C\int \left| Q_1\right|^2 dx +C \int \left| \left(p-\overline{p}\right)_x\right|^2 dx \\ & \quad \leq \frac{1}{64}\bigl\lVert\psi_{1t}\bigr\rVert_{L^2}^2 + C\int \left| Q_1\right|^2 dx + C\int \left| \left(\phi_x,\zeta_x\right)\right|^2 dx \\ & \qquad + C \int \left| \left(\overline{\theta}_x,\overline{v}_x\right)\right|^2 \left| \left(\zeta,\phi\right)\right|^2 dx . \end{aligned} \end{align}\]
By using Young’s inequality, we have
\[\begin{align} \begin{aligned} \int \psi_{1t}\frac{4}{3} \left(\frac{\mu\left(\theta^C\right)u_{1x}^C}{v^C}\right)_x dx \leq & C \int \left| \psi_{1t}\right| \left| \left(u_{1xx}^C,\theta_x^Cu_{1x}^C,u_{1x}^Cv_x^C\right)\right| dx \\ \leq & \frac{1}{64}\bigl\lVert\psi_{1t}\bigr\rVert_{L^2}^2 + C \int \left| Q_1^C\right|^2 dx \end{aligned} \end{align}\] and \[\begin{align} \begin{aligned} \int \psi_{1t} \int \xi_1^2 \widetilde{G}_x d\xi dx \leq & \frac{1}{64}\bigl\lVert\psi_{1t}\bigr\rVert_{L^2}^2 +C \int \left\{\int \xi_1^2 \widetilde{G}_x d\xi\right\}^2 dx\\ \leq & \frac{1}{64}\bigl\lVert\psi_{1t}\bigr\rVert_{L^2}^2 + C \int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 dx. \end{aligned} \end{align}\]
Therefore, we have the following estimate, \[\begin{align} \begin{aligned} \bigl\lVert\psi_{1t}\bigr\rVert_{L^2}^2\leq &C \sum_{i=1,3}\delta_i^3 \left| \dot{X}_i\right|+ C\int \left| \left(\phi_x,\zeta_x\right)\right|^2 dx+C\int \left| Q_1\right|^2 dx+ C \int \left| \left(\overline{\theta}_x,\overline{v}_x\right)\right|^2 \left| \left(\zeta,\phi\right)\right|^2 dx \\ &+C \int \left| Q_1^C\right|^2 dx + C \int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 dx . \end{aligned} \end{align}\]
For the estimate of \(\psi_{it}\), we have
\[\begin{align} \begin{aligned} \int \left| \psi_{it}\right|^2 dx = \bigl\lVert\psi_{it}\bigr\rVert_{L^2}^2, \end{aligned} \end{align}\] and \[\begin{align} \begin{aligned} \int \psi_{it} \int \xi_1\xi_i \widetilde{G}_x d\xi dx \leq& \frac{1}{64}\bigl\lVert\psi_{it}\bigr\rVert_{L^2}^2 + C \int \left\{\int \xi_1\xi_i \widetilde{G}_x d\xi\right\}^2 dx\\ \leq & \frac{1}{64}\bigl\lVert\psi_{it}\bigr\rVert_{L^2}^2 + C \int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 dx. \end{aligned} \end{align}\] Therefore, \[\begin{align} \begin{aligned} \bigl\lVert\psi_{it}\bigr\rVert_{L^2}^2 \leq C \int \bigl\lVert\widetilde{G}_x\bigr\rVert_{\nu,M_\#}^2 dx. \end{aligned} \end{align}\]
To estimate \(\zeta_t\), we can observe \[\begin{align} \begin{aligned} & \int \zeta_t\left(pu_{1x}-p^{S_{1},-X_{1}}\bigl((u_1^{S_{1}})^{-X_{1}}\bigr)_x-p^Cu_{1x}^C-p^{S_{3},-X_{3}}\bigl((u_1^{S_{3}})^{-X_{3}}\bigr)_x\right) dx\\ & \leq \frac{1}{64} \bigl\lVert\zeta_t\bigr\rVert_{L^2}^2 + C \int \left| Q_2\right|^2 dx + \int \left| \left(pu_{1x}-\overline{p}\overline{u}_{1x}\right)\right|^2 dx\\ & \leq \frac{1}{64} \bigl\lVert\zeta_t\bigr\rVert_{L^2}^2 + C \int \left| Q_2\right|^2 dx + C \int \left| \psi_{1x}\right|^2 dx + C \int \left| \overline{u}_{1x}\right|^2\left| \left(\phi,\zeta\right)\right|^2 dx. \end{aligned} \end{align}\] Furthermore, \(\bigl\lVert\theta_{xx}^C\bigr\rVert_{L^2}^2\) is globally time integrable since its time decay is \((1+t)^{-3/2}\) we have the following inequality,
\[\begin{align} \begin{aligned} & \int \zeta_t \left(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right)\int \xi_1^2 \bigl((G^{S_{i}})^{-X_{i}}\bigr)_x d\xi dx \\ & \qquad \leq \frac{1}{64} \bigl\lVert\zeta_t\bigr\rVert_{L^2}^2 + C\int \left(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right)^2 \left\{\int \xi_1^2 \bigl((G^{S_{i}})^{-X_{i}}\bigr)_x d\xi\right\}^2 dx\\ & \qquad \leq \frac{1}{64} \bigl\lVert\zeta_t\bigr\rVert_{L^2}^2 + C\int \left(u_1-\bigl(u_1^{S_{i}}\bigr)^{-X_{i}}\right)^2 \left| \bigl((v^{S_{i}})^{-X_{i}}\bigr)_x\right|^2 dx. \end{aligned} \end{align}\]
The other terms are computed by the similar method of the estimate of \(\psi_{1t}\). ◻
Proof. Using the same method as [38], it holds that \[\begin{align} &\left(\frac{\overline{p}\theta}{2v}\phi_x^2+\frac{3\overline{p}v}{4}\psi_{1x}^2+\sum_{k=2}^3\frac{\psi_{kx}^2}{2}+\frac{\zeta_x^2}{2}\right)_t+2\overline{p}\psi_{1xx}^2\mu\left(\overline{\theta}\right)+\sum_{k=2}^3\frac{\mu(\theta)}{v}\psi_{kxx}^2+\frac{\alpha_{\rm{th}}\left(\overline{\theta}\right)}{v}\zeta_{xx}^2\\ &=-\sum_{i=1,3}\dot{X}_i\left[\phi_{xx}\bigl((v^{S_{i}})^{-X_{i}}\bigr)_x\frac{\overline{p}\theta}{v}+\psi_{1xx}\bigl((u_1^{S_{i}})^{-X_{i}}\bigr)_x\frac{3\overline{p}v}{2}+\zeta_{xx}\bigl((\theta^{S_{i}})^{-X_{i}}\bigr)_x\right]+\frac{\phi_x^2}{2}\left(\frac{\overline{p}\theta}{v}\right)_t\\ &+\frac{\psi_{1x}^2}{2}\left(\frac{3\overline{p}v}{2}\right)_t-\left(\frac{\overline{p}\theta}{v}\right)_x\phi_x\phi_t+\left(\frac{\overline{p}\theta}{v}\right)_x\phi_x\psi_{1x}-\left(\frac{3\overline{p}v}{2}\right)_x\psi_{1x}\psi_{1t}+\psi_{1xx}\overline{p}v\overline{\theta}_x\left(\frac{1}{v}-\frac{1}{\overline{v}}\right)\\ &-\psi_{1xx}\overline{p}v\overline{v}_x\left(\frac{\theta}{v^2}-\frac{\overline{\theta}}{\overline{v}^2}\right)-\psi_{1x}\overline{p}_x\zeta_x+\zeta_{xx}u_{1x}\left(p-\overline{p}\right)-2\overline{p}v\psi_{1xx}\left(\left(\mu(\theta)-\mu\left(\overline{\theta}\right)\right)\frac{u_{1x}}{v}\right)_x\\ &-2\overline{p}v\psi_{1xx}\left[\left(\mu\left(\overline{\theta}\right)\right)_x\left(\frac{u_{1x}}{v}-\frac{\overline{u}_{1x}}{\overline{v}}\right)-\mu\left(\overline{\theta}\right)\frac{v_x}{v^2}\psi_{1x}+\mu\left(\overline{\theta}\right)\left\{\overline{u}_{1x}\left(\frac{1}{v}-\frac{1}{\overline{v}}\right)\right\}_x\right]\\ &-\zeta_{xx}\left(\left(\alpha_{\rm{th}}(\theta)-\alpha_{\rm{th}}\left(\overline{\theta}\right)\right)\frac{\theta_x}{v}\right)_x+\sum_{k=2}^3\frac{\psi_{kx}^2}{2}\left(\frac{\mu(\theta)}{v}\right)_{xx}-\zeta_{xx}\sum_{k=2}^3\frac{\mu(\theta)}{v}\psi_{kx}^2+\zeta_{xx}Q_2\\ &+\psi_{1xx}\frac{3\overline{p}v}{2}Q_1 -\zeta_{xx}\left[\left(\alpha_{\rm{th}}\left(\overline{\theta}\right)\right)_x\left(\frac{\theta_{x}}{v}-\frac{\overline{\theta}_{x}}{\overline{v}}\right)-\alpha_{\rm{th}}\left(\overline{\theta}\right)\frac{v_x}{v^2}\zeta_{x}+\alpha_{\rm{th}}\left(\overline{\theta}\right)\left\{\overline{\theta}_{x}\left(\frac{1}{v}-\frac{1}{\overline{v}}\right)\right\}_x\right]\\ &-\frac{4}{3}\zeta_{xx}\left(\frac{\mu(\theta)u_{1x}^2}{v}-\frac{\mu\left(\overline{\theta}\right)\overline{u}_{1x}^2}{\overline{v}}\right)+\psi_{1xx}\frac{3\overline{p}v}{2}\int \xi_1^2 \widetilde{\Pi}_{1x} d\xi +\sum_{k=2}^3 \psi_{kxx}\int \xi_1\xi_i \Pi_{1x}d\xi\\ & + \zeta_{xx}\int \xi_1 \frac{\left| \xi\right|^2}{2}\widetilde{\Pi}_{1x} d\xi - \zeta_{xx}\sum_{k=2}^3 \psi_k\int \xi_1\xi_i \Pi_{1x}d\xi\\ &-\zeta_{xx}\left[u_1\int \xi_1^2 \Pi_{1x}d\xi-\bigl(u_1^{S_{1}}\bigr)^{-X_{1}}\int\xi_1^2 \bigl((\Pi_1^{S_{1}})^{-X_{1}}\bigr)_xd\xi -\bigl(u_1^{S_{3}}\bigr)^{-X_{3}}\int \xi_1^2 \bigl((\Pi_1^{S_{3}})^{-X_{3}}\bigr)_xd\xi\right]\\ &+ (\mathcal{R}^{(1)})_x. \end{align}\] Here \(\mathcal{R}^{(1)}\) denotes a collection of lower-order flux terms produced by integration by parts and differentiation of the coefficients. Since the estimate is carried out over \(\mathbb{R}_x\), these divergence terms do not contribute after integration in \(x\).
Collecting the above identity, estimating the fluid error terms as in the zeroth-order energy argument, and controlling the microscopic terms by the auxiliary estimates from the high-order microscopic analysis, we obtain ?? . ◻
Acknowledgment. MC and MJK were partially supported by the National Research Foundation of Korea (RS-2024-00361663 and NRF-2019R1A5A1028324). CK is partially supported by NSF-CAREER 2047681. This material is partly based upon work supported by the National Science Foundation under Grant No. DMS-2424139, while one of the authors (C.K.) was in residence at the Simons Laufer Mathematical Sciences Institute in Berkeley, California, during the Fall 2025 semester.↩︎
This viewpoint should be regarded as stronger than the standard smooth-limit theory. The author argues, by a shock-scaling consideration, that in nonsmooth hydrodynamics “there is no concept of ‘small’ or ‘negligible’ higher derivative terms” [13]. In a later formulation, he states that “Hilbert’s program will fail because of the appearance of van der Waals–Korteweg capillarity terms” [15]. We cite this as a critical viewpoint, rather than as a settled consensus on the Boltzmann–Euler limit.↩︎