Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects
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American Institute of Aeronautics and Astronautics
Reference20 articles.
1. The joined wing - An overview
2. Structural Weight Comparison of a Joined Wing and a Conventional Wing
3. Selberg, B. P. and Cronin, D. L. "Aerodynamic-Structural Optimization of Positive/Negative Stagger Joined Wing Configurations," AIAA Paper 86-2626, AIAA/AHS/ASEE Aircraft Systems, Design and TechnologyMeeting, Dayton, Ohio, 20-22,Oct. 1986.
4. Hajela, P. and Chen, J.L. "Optimum Structural Sizing of Conventional Cantilever and Joined-Wing Configurations Using Equivalent Beam Models," AIAA Paper 86-2653, AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting, Dayton, Ohio, 20-22,Oct. 1986.
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