Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of Attack
Author:
Affiliation:
1. North American Aviation, Inc.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2149
Reference7 articles.
1. Das Umstr�mungsproblem bei inkompressiblen Potentialstr�mungen
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