Shock Wave/ Boundary-Layer Interaction Control Using Streamwise Slots in Transonic Flows
- 1 May 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 41 (3), 540-546
- https://doi.org/10.2514/1.11479
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
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