2006
DOI: 10.1016/j.jmaa.2006.02.044
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Global classical solutions for a free-boundary problem modeling combustion of solid propellants

Abstract: We study a free-boundary problem for the heat equation in one space dimension, describing the burning of a semi-infinite adiabatic solid propellant subjected to external thermal radiation (typically, a laser). The model includes the presence on the moving solid-gas interface (the free boundary) of heat release, due both to propellant degradation and conductive heat feedback from the gas phase reactions. The pyrolysis law and the flame submodel, relating burning rate to the boundary temperature and the heat fee… Show more

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Cited by 1 publication
(4 citation statements)
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“…Indeed, considering the estimates in more detail, we obtain as a consequence of Lemma 4.1 in [9] that there exists a constant K = K (t) > 0 depending on t but independent of u 0 such that…”
Section: Lemma 32mentioning
confidence: 96%
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“…Indeed, considering the estimates in more detail, we obtain as a consequence of Lemma 4.1 in [9] that there exists a constant K = K (t) > 0 depending on t but independent of u 0 such that…”
Section: Lemma 32mentioning
confidence: 96%
“…Then a function u = u (x, t) is a (classical global) solution of problem (1) if (1) hold. Existence and uniqueness was established in [9]: Theorem 2.1. We assume that the hypothesis H1 is satisfied.…”
Section: The Semigroupmentioning
confidence: 99%
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