Fluctuating Loads in Shock Wave/Turbulent Boundary Layer Interaction: Tutorial and Update
Author:
Affiliation:
1. The University of Texas at Austin, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-284
Reference112 articles.
1. Physical model of the swept shock wave/boundary-layer interaction flowfield
2. Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flows
3. The structure of aerodynamic heating in three-dimensional shock wave/turbulent boundary layer interactions induced by sharp and blunt fins
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