Supersonic Corner Flow Predictions Using the Quadratic Constitutive Relation
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7512
2. Purdue University, West Lafayette, Indiana 47907-2045
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054732
Reference46 articles.
1. PrandtlL. “Turbulent Flow,” NACA TR TM-435, Sept. 1926.
2. Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section
3. Flow dynamics past a simplified wing body junction
4. Further experiments on supersonic turbulent flow development in a square duct
5. Control of Supersonic Inlet-Isolator Unstart Using Active and Passive Vortex Generators
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