Calculation of three-dimensional shock/turbulent boundary-layer interaction generated by sharp fin
Author:
Affiliation:
1. Rutgers, The State University of New Jersey, New Brunswick, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9192
Reference28 articles.
1. Interactions between shock waves and turbulent boundary layers
2. 2Hankey, W. and Holden, M. " Two-Dimensional Shock Wave-Boundary Layer Interactions in High Speed Flows," AGARDograph No. 203, June 1975.
3. Flow Lasers
4. A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equations
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