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DIRECTED ENERGY PROFESSIONAL SOCIETY

Abstract: 26-Symp-004

UNCLASSIFIED, PUBLIC RELEASE

Numerical Analysis of Inlet Distortion on a Hypersonic Engine

Numerical simulations were performed to understand the impact of a damaged scramjet inlet on the operability and performance of the combustor, in terms of pressure rise and thrust, with different fueling schemes.

UNCLASSIFIED, PUBLIC RELEASE

 
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