Introduction and Formulation of the Problem
Until recently the numerical and analytical investigations of the steady combustion of gas mixtures at supersonic speeds were carried out under the assumption of one-dimensional flow behind a normal shock wave or quasi-one-dimensional flow in a stream tube with given cross-section variations or with given variations of one flow parameter (for instance, at constant pressure).
KeywordsShock Wave Steady Flow Supersonic Flow Stream Tube Normal Shock Wave
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