Numerical Method for Hypersonic Internal Flow over Blunt Leading Edges and Two Blunt Bodies
- 1 May 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (5) , 617-622
- https://doi.org/10.2514/3.50165
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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