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[American Institute of Aeronautics and Astronautics 37th AIAA Fluid Dynamics Conference and Exhibit - Miami, Florida ()] 37th AIAA Fluid Dynamics Conference and Exhibit - Wall-Pressure Measurements in a Mach 3 Shock-Wave Turbulent Boundary Layer Interaction at a DNS Accessible Reynolds Number

✍ Scribed by Ringuette, Matthew; Smits, Alexander


Book ID
121065957
Publisher
American Institute of Aeronautics and Astronautics
Year
2007
Tongue
English
Weight
941 KB
Category
Article
ISBN
1624100082

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