Effect of nose bluntness and cone angle on slender-vehicle transition
- 1 October 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (10) , 1168-1174
- https://doi.org/10.2514/3.10024
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
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