Compatibility relations and a generalized finite-difference approximation for three- dimensional steady supersonic flow.
Author:
Affiliation:
1. Northrop Norair, Hawthorne, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4006
Reference20 articles.
1. An Initial Value Problem for all Hyperbolic Partial Differential Equations of Second Order with Three Independent Variables
2. The method of characteristics in the three-dimensional stationary supersonic flow of a compressible gas
3. G. The Method of Characteristics
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