Multi-Fidelity Computational Investigations of Hypersonic Shock Wave-Boundary Layer Interactions in a Multi-Compression Scramjet Inlet
AIAA SciTech Forum ; 2023 ; National Harbor, Md.; Online
High-speed air-breathing propulsion ; 127-142
2023
Aufsatz (Konferenz)
Englisch
BKL: | 55.50 Luftfahrzeugtechnik |
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AIAA | 2017
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