Hypersonic Studies of the Leading Edge Effect on the Flow Over a Flat Plate
Author:
Affiliation:
1. Forrestal Research Center, Princeton University, Princeton, N. J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.6969
Reference23 articles.
1. On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate Solutions
2. Hypersonic Viscous Flow over an Inclined Wedge
3. Superaerodynamics, Mechanics of Rarefied Gases
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