2007
DOI: 10.1016/j.jde.2006.10.006
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Pointwise Green function bounds and stability of combustion waves

Abstract: Generalizing similar results for viscous shock and relaxation waves, we establish sharp pointwise Green function bounds and linearized and nonlinear stability for traveling wave solutions of an abstract viscous combustion model including both Majda's model and the full reacting compressible Navier-Stokes equations with artificial viscosity with general multi-species reaction and reaction-dependent equation of state, under the necessary conditions of strong spectral stability, i.e., stable point spectrum of the… Show more

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Cited by 25 publications
(35 citation statements)
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References 45 publications
(195 reference statements)
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“…A detailed overview of these results can be found in the recent work of Humpherys et al [17]. Notably, however, outside of the Evans-function framework, namely [22,23], we know of no stability results for weak-detonation solutions of the Majda model.…”
Section: 2mentioning
confidence: 99%
See 1 more Smart Citation
“…A detailed overview of these results can be found in the recent work of Humpherys et al [17]. Notably, however, outside of the Evans-function framework, namely [22,23], we know of no stability results for weak-detonation solutions of the Majda model.…”
Section: 2mentioning
confidence: 99%
“…To describe our results more precisely, we now introduce the version of the Majda model to which will be the setting for our analysis 2 . We begin with the Majda model [22]:…”
mentioning
confidence: 99%
“…Proposition 1 (Lyng-Raoofi-Texier-Zumbrun [42]). Under the Evans-function condition E(·) has precisely one zero in {Re λ ≥ 0} (necessarily at λ = 0) ,…”
Section: Stabilitymentioning
confidence: 99%
“…Basic Assumptions. Following Lyng, Raoofi, Texier & Zumbrun [42], we begin with the following version of the Majda model:…”
Section: Preliminariesmentioning
confidence: 99%
“…New physical applications beyond those of [10] are to undercompressive waves in MHD and, with slight modification following [16], to weak detonation waves in reactive compressible Navier-Stokes equations. The latter we intend to treat in a future work.…”
Section: Definition 12 An Ideal Shockmentioning
confidence: 99%