The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic Speeds
Author:
Affiliation:
1. North American Aviation, Inc.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.8501
Reference4 articles.
1. Experiments on Boundary-Layer Transition at Supersonic Speeds
2. Stress Analysis of Sheet-Stringer Panels with Cutouts
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