Boundary-Layer Measurements in Hypersonic Flow
Author:
Affiliation:
1. The Johns Hopkins University,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3498
Reference20 articles.
1. Turbulent Boundary Layers in Adverse Pressure Gradients
2. Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic Velocities
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