Supersonic autoignitive reaction waves are shown to be equivalent to Rayleigh flow and therefore to weak detonations, with realization conditions of inlet velocity above the Chapman-Jouguet speed and autoignition within the domain.
Aerial plane waves of finite amplitudes
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Weak Detonations Revisited: Uncovering Its General Nature Using Autoignitive Reaction Wave Concept
Supersonic autoignitive reaction waves are shown to be equivalent to Rayleigh flow and therefore to weak detonations, with realization conditions of inlet velocity above the Chapman-Jouguet speed and autoignition within the domain.