Laminar boundary layer on a cone at incidence in supersonic flow
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (3), 462-468
- https://doi.org/10.2514/3.6203
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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