Linear Stability Theory of Detonation Wave with Two-Front Structure
Let us consider again the one-dimensional gas flow with plane detonation wave having two-front structure (Fig. 1). The variations of velocity, pressure and density of the gas in each of the three regions, separated one of the other by adiabatic shock פ and heat release front f are described by equations of adiabatic gas flow (Pt. 1, Eqs (2.1)). Let the subscript ∞ denote the values ahead of adiabatic shock, the subscript 1 — the values inside the layer between two fronts, and let the values behind the heat release front be without any subscripts.
KeywordsShock Wave Heat Release Detonation Wave Induction Time Combustion Front
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