One concept for hypersonic air-breathing propulsion is a detonation-combustion RAMJET, in which fuel added to the air burns in a detonation wave. As a simplified model for analysis of such a device, assume that the standing detonation can be modeled as a normal shock wave followed by a region of constant-area heat addition that
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One concept for hypersonic air-breathing propulsion is a detonation-combustion RAMJET, in which fuel...
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