Research Progress of Hypersonic Inlet Inverse Design Based on Curved Shock Compression System
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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Online Contents | 2014
|OPTIMIZATION AND EXPERIMENTAL INVESTIGATION OF 2-D HYPERSONIC CURVED SHOCK COMPRESSION INLET
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