Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition
Author:
Affiliation:
1. California Institute of Technology, Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1974-133
Reference26 articles.
1. i Tech. Rept. AFFDL-TR-68-149,March, 1969.
2. Berlin, 1958.
3. Aerodynamic Noise in Supersonic Wind Tunnels
4. Some Statistical Properties of the Pressure Field Radiated by a Turbulent Boundary Layer
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