Theoretical Determination of the Minimum Drag of Airfoils at Supersonic Speeds
Author:
Affiliation:
1. Ames Aeronautical Laboratory, N.A.C.A.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2493
Reference23 articles.
1. The Minimum Drag of Thin Wings in Frictionless Flow
2. Whittaker, E. T., and Watson, G. N., Modern Analysis, pp.388-403; The Macmillan Company, New York, 1945.
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