Nozzle Wall Boundary Layers at Mach Numbers 20 to 47
- 1 July 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (7) , 872-879
- https://doi.org/10.2514/3.50239
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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