Three-dimensional shock wave-turbulent boundary layer interactions generated by a sharp fin at Mach 4
Author:
Affiliation:
1. Rutgers University, New Brunswick, NJ
2. NASA, Ames Research Center, Moffett Field, CA
3. Pennsylvania State University, University Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-648
Reference11 articles.
1. gKnight, D. "Calculation of Three-Dimensional ShockRurbulent Boundarv 1056-1061.
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