Experimental Study of Hypersonic Flutter of a Blunt-leading-edge Trapezoidal Wing
21st AIAA International Space Planes and Hypersonics Technologies Conference
2017-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Experimental Study of Hypersonic Flutter of a Blunt-leading-edge Trapezoidal Wing (AIAA 2017-2180)
British Library Conference Proceedings | 2017
|Drag of blunt leading edge of swept wing in hypersonic flow
Engineering Index Backfile | 1964
|THE BLUNT-LEADING-EDGE PROBLEM IN HYPERSONIC FLOW
AIAA | 1963
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