Experimental and computational study of a swept compression corner interaction flowfield
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania
2. NASA Ames Research Center, Moffett Field, California
3. Princeton University, Princeton, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9341
Reference23 articles.
1. Interactions between shock waves and turbulent boundary layers
2. Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression Corners
3. Cylindrical and conical flow regimes of three-dimensional shock/boundary-layer interactions
4. Conical similarity of shock/boundary-layer interactions generated byswept and unswept fins
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