Transonic shock-wave/turbulent boundary-layer interactions in a circular duct
Author:
Affiliation:
1. University of Washington, Seattle, Washington
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8974
Reference27 articles.
1. 4Gadd, G. E. "Interactions Between Normal Shock Waves and Turbulent Boundary Layers," ARC R&M 3262, Feb.1961.
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