Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference51 articles.
1. Bemerkungen über die Entstehung der Turbulenz
2. Schlichting, H., Boundary Layer Theory, 6th ed.,McGraw-Hill,New York, 1968, pp.431-522.
3. Schubauer, G. B. and Skramstad, H. K. "Laminar-Boundary-Layer Oscillations and Transition on a Flat Plate," Rept. 909,1948, NACA.
4. Effects of freestream disturbances on boundary-layer transition.
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