Analysis and Design of a Morphing Wing Tip using Multicellular Flexible Matrix Composite Adaptive Skins
The material presented in this thesis uses concepts of the finite element and doublet panel methods to develop a structural-aerodynamic coupled mathematical model for the analysis of a morphing wing tip composed of smart materials. Much research is currently being performed within many facets of eng...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/33932 http://scholar.lib.vt.edu/theses/available/etd-07082009-140914/ |