Impact of Ramped Vanes on Normal Shock Boundary Layer Interaction
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
2. University of Virginia, Charlottesville, Virginia 22904
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051253
Reference63 articles.
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5. Large-scale motions in a supersonic turbulent boundary layer
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