Effects of nose bluntness, angle of attack, and oscillation amplitude on hypersonic unsteady aerodynamics of slender cones
- 1 February 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (2) , 297-304
- https://doi.org/10.2514/3.6166
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
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