Computational Fluid Dynamics Study of Optimized Hypersonic Leading Edge Geometries
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
2015-01-01
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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