Two- and three-dimensional effects in the supersonic mixing layer
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11016
Reference31 articles.
1. Compressibility Effects in Turbulent Shear Layers
2. The compressible turbulent shear layer: an experimental study
3. Spreading of two-stream supersonic turbulent mixing layers
4. Compressibility effects in free shear layers
5. Velocity measurements of compressible turbulent mixing layers
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