Koiter–Newton Based Model Reduction for Large Deflection Analysis of Wing Structures
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DOI: 10.2514/1.j062514
Abstract: Wing structures subjected to large deflections are prone to nonlinear load-deflection behavior. Geometric nonlinearities can arise due to the accompanying large rotations and in-plane deflections that manifest in the form of stiffening effects in the… read more here.
Keywords: wing structures; deflection; large deflection; model ... See more keywords