Wall cooling effects on hypersonic transitional/turbulent boundary layers at high Reynolds numbers
- 1 October 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (10), 1455-1461
- https://doi.org/10.2514/3.7440
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
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