Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactions
- 1 November 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (11) , 1907-1920
- https://doi.org/10.2514/3.2700
Abstract
No abstract availableKeywords
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