Optimal Problem Definition for Optimization of Morphing Structures
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American Institute of Aeronautics and Astronautics
Reference23 articles.
1. 2Anderson, G., Cowan, D., and Piatak, D. “Aeroelastic Modelling. Analysis and Testing of a Morphing Wing Structure,” Inproc 48th AIAA Structures, Structural Dynamics, and Materials Conference, Vol. AIAA 2007-1734, 2007.
2. 4Blondeau, J., Richeson, J., and Pines, D. “Design, development and testing of a morphing aspect ratio wing using an inflatable telescopic spar,” Inproc 44th AIAA Structures, Structural Dynamics, and Materials Conference, Vol. AIAA 2003-1718, 2003.
3. 5Gano, S., Perez, V., Renaud, J., Batill, S., and Sanders, B. “Multi-level Variable Fidelity Optimization of a Morphing Unmanned Aerial Vehicle,” Inproc 45th AIAA Structures, Structural Dynamics, and Materials Conference, Vol. AIAA 2004-1763, 2004.
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