Unsteady pressure loads generated by swept-shock-wave/boundary-layer interactions
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference28 articles.
1. Fluctuating Wall Pressure under a Separated Supersonic Flow
2. 3Dolling, D. S., and Bogdonoff, S. M. "An Experimental Investigation of the Unsteady Behavior of Blunt Fin-Induced Shock Wave Turbulent Boundary Layer Interactions "AIAA Paper 81-1287, June 1981.
3. Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield
4. Unsteadiness of the shock wave structure in attached and separated compression ramp flows
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