Computational Fluid Dynamics Study of Optimized Hypersonic Leading Edge Geometries
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Computational Fluid Dynamics Study of Optimized Hypersonic Leading Edge Geometries (AIAA 2015-3509)
British Library Conference Proceedings | 2015
|The hypersonic leading-edge problem
AIAA | 1968
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