Structural optimization for joined-wing synthesis
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46924
Reference10 articles.
1. Computation of induced drag for elliptical and crescent-shaped wings
2. Structural Weight Comparison of a Joined Wing and a Conventional Wing
3. Parametric weight evaluation of joined wings by structural optimization
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