Multiple transonic shock-wave/turbulent boundary-layer interaction in a circular duct
- 1 October 1985
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (10) , 1506-1511
- https://doi.org/10.2514/3.9117
Abstract
No abstract availableKeywords
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