A Quasi-Vortex-Lattice Method in Thin Wing Theory
Author:
Affiliation:
1. The University of Kansas, Lawrence, Kan.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60381
Reference16 articles.
1. Comment on " Span wise Distribution of Induced Drag in Subsonic Flow by the Vortex Lattice Method"
2. Remarks on vortex-lattice methods.
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