Mitigation of pressure oscillations induced by supersonic flow over slender cavities
- 1 November 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 29 (6) , 999-1004
- https://doi.org/10.2514/3.46276
Abstract
No abstract availableKeywords
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