Theoretical Pressure Recovery Through a Normal Shock in a Duct with Initial Boundary Layer
- 1 March 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (3) , 169-174
- https://doi.org/10.2514/8.2582
Abstract
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