Transitional boundary-layer considerations for the heating analyses of lifting re-entry vehicles.
- 1 September 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 6 (9) , 1048-1053
- https://doi.org/10.2514/3.29754
Abstract
No abstract availableKeywords
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