Numerical optimization design of advanced transonic wing configurations
Author:
Affiliation:
1. General Dynamics Corp., Convair Div., San Diego, CA; Colorado, University, Boulder, CO
2. NASA, Ames Research Center, Applied Computational Aerodynamics Branch, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-424
Reference16 articles.
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