Physical model of the swept shock wave/boundary-layer interaction flowfield
- 1 September 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (9), 2252-2258
- https://doi.org/10.2514/3.11212
Abstract
No abstract availableKeywords
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