ME 4015: Hy-V SCRamjet Design Project

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The design process incorporated different state
of the art computer software
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CFD simulation validated predicted combustor flow
conditions exited by the Cavity
Distribution of mach number simulated by FLUENT
6.3
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CFD simulation validated predicted combustor flow
conditions exited by the Cavity
Distribution of static temperature simulated by
FLUENT 6.3
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