Wall Drag in Internal Mach-2 Flow with Cavity and Transpiration Injection
Author:
Affiliation:
1. University of Washington, Seattle, Washington 98195
2. NASA Langley Research Center, Hampton, Virginia 23681
3. University of Arkansas, Fayetteville, Arkansas 72701
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5592
Reference21 articles.
1. Schlicting,H., BoundaryLayer Theory, McGraw- Hill, New York, 1968, pp.597-606.
2. Direct Measurement of Supersonic Skin Friction
3. Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic Flow
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