An iterative procedure for three-dimensional transonic wing design by the integral equation method
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-2155
Reference12 articles.
1. Transonic Flows for Aircraft with Nacells, Pylons, and Winglets,'' A T M Paper No.80-0130, 1980.
2. Method,'' Journal of Aircraft Vol.18, No.2, 1981.
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