Flow visualization methods for separated three-dimensional shock wave/turbulent boundary-layer interactions
- 1 March 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (3), 390-397
- https://doi.org/10.2514/3.8085
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
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