Flow Properties of a Supersonic Turbulent Boundary Layer with Wall Roughness
Author:
Affiliation:
1. Air Force Institute of Technology, Wright – Patterson Air Force Base, Ohio 45433-7765
2. University of Alabama, Tuscaloosa, Alabama 35487-0280
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.862
Reference37 articles.
1. A generalized correlation of roughness density effects on the turbulent boundary layer.
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