Effect of Nose Bluntness on Fin-Cone Transition at Mach 6
AIAA AVIATION 2021 FORUM
01.01.2021
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of nose bluntness on transition for cone and hollow cylinder at Mach numbers 1.41 and 2.01
Engineering Index Backfile | 1961
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