Experimental Evaluation of Heat Transfer with Transpiration Cooling in a Turbulent Boundary Layer at M = 3.2
Author:
Affiliation:
1. Convair Scientific Research Laboratory, San Diego, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.8397
Reference17 articles.
1. A Note on Blast-Wave Theory
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