By a combination of asymptotic ODE estimates and numerical Evans function calculations, we establish stability of viscous shock solutions of the isentropic compressible Navier-Stokes equations with γ-law pressure (i) in the limit as Mach number M goes to infinity, for any γ ≥ 1 (proved analytically), and (ii) for M ≥ 2, 500, γ ∈ [1, 2.5] (demonstrated numerically). This builds on and completes earlier studies by Matsumura-Nishihara and Barker-Humpherys-Rudd-Zumbrun establishing stability for low and intermediate Mach numbers, respectively, indicating unconditional stability, independent of shock amplitude, of viscous shock waves for γ-law gas dynamics in the range γ ∈ [1, 2.5]. Other γ-values may be treated similarly, but have not been checked numerically. The main idea is to establish convergence of the Evans function in the high-Mach number limit to that of a pressureless, or "infinitely compressible", gas with additional upstream boundary condition determined by a boundarylayer analysis. Recall that low-Mach number behavior is incompressible.1 The result of [21] is obtained by energy estimates combining the techniques of [34] with those of [14,15]; a similar approach has been used in [30] to obtain smallamplitude zero-mass stability of Boltzmann shocks. See [37,12] for an alternative approach based on asymptotic ODE methods. Stability of isentropic viscous shock profiles 3[34], in fact yields stability of small-amplitude shocks of general symmetric hyperbolic-parabolic systems, largely settling the problem of small-amplitude shock stability for continuum mechanical systems.However, there remains the interesting question of large-amplitude stability. The main result in this direction, following a general strategy proposed in [47], is a "refined Lyapunov theorem" 2 established by Mascia and Zumbrun [32,46] for general symmetric hyperbolicparabolic systems, stating that linearized and nonlinear L 1 ∩ H 3 → L 1 ∩ H 3 orbital stability (the standard notions of stability) are equivalent to spectral stability, or nonexistence of nonstable (nonnegative real part) eigenvalues of the linearized operator L about the wave, other than the single zero eigenvalue arising through translational invariance of the underlying equations.This reduces the problem of large-amplitude stability to the study of the associated eigenvalue equation (L−λ)u = 0, a standard analytically and numerically well-posed (boundary value) problem in ODE, which can be attacked by the large body of techniques developed for asymptotic, exact, and numerical study of ODE. In particular, there exist well-developed and efficient numerical algorithms to determine the number of unstable roots for any specific linearized operator L, independent of its origins in the PDE setting; see, e.g., [9,10,11,8,22] and references therein. In this sense, the problem of determining stability of any single wave is satisfactorily resolved, or, for that matter, of any compact family of waves. To determine stability of a family of waves across an unbounded parameter regime, how...
Abstract. This paper deals with the modelling of the coolant (water) in a nuclear reactor core. This study is based on a monophasic low Mach number model (Lmnc model) coupled to the stiffened gas law for a single-phase flow. Some analytical steady and unsteady solutions are presented for the 1D case. We then introduce a numerical scheme to simulate the 1D model in order to assess its relevance. Finally, we carry out a normal mode perturbation analysis in order to approximate 2D solutions around the 1D steady solutions.Résumé. Dans cet article, nous nous intéressonsà la modélisation de l'écoulement de l'eau dans le circuit primaire d'un réacteur nucléaire. Pour cela, nous utilisons un modèle bas-Mach monophasique (modèle Lmnc) pour une loi d'état de type gaz raidi. Nous présentons des solutions analytiques 1D stationnaires et instationnaires pour certains types de données. Nous simulons ensuite le modèle afin d'évaluer sa pertinence. La dernière partie est consacréeà une analyse de pertubations en modes normaux réalisée pour approcher les solutions 2Dà partir des solutions stationnaires 1D.
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.
customersupport@researchsolutions.com
10624 S. Eastern Ave., Ste. A-614
Henderson, NV 89052, USA
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.
Copyright © 2024 scite LLC. All rights reserved.
Made with 💙 for researchers
Part of the Research Solutions Family.