Structure of a Supersonic Three-Dimensional Cylinder/Offset-Flare Turbulent Interaction
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7913
2. North Carolina State University, Raleigh, North Carolina 27695
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3232
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1. Progress in shock wave/boundary layer interactions;Progress in Aerospace Sciences;2015-01
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3. Mean Flowfield Structure of a Supersonic Three-Dimensional Base Flow;Journal of Aircraft;2010-03
4. Development of some hypersonic benchmark flows using CFD and experiment;Shock Waves;2003-03-01
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