Numerical Procedure for the Computation of Irrotational Conical Flows
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61234
Reference40 articles.
1. The lift of a delta wing at supersonic speeds
2. SUPERSONIC FLOW PAST SLENDER POINTED BODIES
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