Abstract:Compared to pulse detonation engine and rotating detonation engine, oblique detonation engine has the advantage in higher flight Mach number. However, it is still challenging to achieve stabilized oblique detonation wave for a broad range of flight conditions. To control oblique detonation wave, this study focuses on the oblique detonation wave structure evolution induced by changing the wedge angle. Transient two-dimensional simulations are conducted for wedge-stabilized oblique detonation wave in stoichiomet… Show more
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