Heat transfer measurements and computations of swept-shock-wave/boundary-layer interactions
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12045
Reference38 articles.
1. Computation of sharp-fin-induced shock wave/turbulent boundary-layerinteractions
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3. Calculation of three-dimensional shock/turbulent boundary-layer interaction generated by sharp fin
4. On the quasi-conical flowfield structure of the swept shock wave-turbulent boundary layer interaction
5. Three-dimensional shock wave-turbulent boundary layer interactions generated by a sharp fin at Mach 4
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