Three-dimensional boundary-layer transition on a swept wing at Mach 3.5
- 1 November 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (11) , 2032-2037
- https://doi.org/10.2514/3.12944
Abstract
No abstract availableKeywords
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