A lower bound for three-dimensional turbulent separation in supersonic flow
Author:
Affiliation:
1. National Research Council, Washington, D. C.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8938
Reference3 articles.
1. Comparison of Shock-Induced Two- and Three- Dimensional Incipient Turbulent Seperation
2. A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock Wave
3. Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners
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