Browse Topic: Carbon nanotubes

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This work presents a structural design optimization of composite rotor blades for a typical unmanned helicopter. Multiple parameters that influence the stiffness and weight of the rotor blade are considered as design variables. These include the number of composite plies, the thickness of composite plies, and the web location as a fraction of the rotor blade airfoil chord. To further improve the stiffness, carbon nano-tubes are doped into the composite material and the percentage of doped carbon nano-tubes are considered as an additional design variable. The structural analysis of the rotor blade is carried out using principle of the Variational Asymptotic Method (VAM). Using VAM, the 3D elastic rotor blade problem is decoupled into two reduced-dimension sequential problems of 2D cross-sectional analysis and 1D beam analysis. Variational Asymptotic Beam Sectional Analysis (VABS) tool is used for the 2D cross-section analysis to obtain the blade stiffness. Orthogonal array based design
Dandinasivara, AbhiramGanguli, RanjanHarursampath, Dineshkumar
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