Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads
Author:
Affiliation:
1. U.S. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7765
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.33428
Reference28 articles.
1. The joined wing - An overview
2. Parametric weight evaluation of joined wings by structural optimization
3. Structural optimization for joined-wing synthesis
4. Joined-Wing Aeroelastic Design with Geometric Nonlinearity
5. A Joined-Wing Structural Weight Modeling Study
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