Numerical Solution for Three-Dimensional Inviscid Supersonic Flow
Author:
Affiliation:
1. Lockheed Palo Alto Research Laboratory, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50241
Reference14 articles.
1. Three-Dimensional Flow around Blunt Bodies
2. Unsteady solution of the flowfield over concave bodies.
3. Compatibility relations and a generalized finite-difference approximation for three- dimensional steady supersonic flow.
4. Theoretical and experimental study of supersonic steady flow around inclined bodies of revolution
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