Unraveling Flow Transition: Experimental Insights into Mach, Reynolds, and Bluntness Variations on a Cone-Cylinder Flare Model
AIAA AVIATION FORUM AND ASCEND 2024
2024-01-01
Conference paper
Electronic Resource
English
Nosetip Bluntness Effects on the ROTEX-T Cone-Flare
AIAA | 2024
|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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