Mach number effects on conical surface features of swept shock-wave/boundary-layer interactions
- 1 January 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (1) , 91-97
- https://doi.org/10.2514/3.10357
Abstract
No abstract availableThis publication has 17 references indexed in Scilit:
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