Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation
This research explores the impact of kinematic structural nonlinearities on the dynamics of a highly deformable cantilevered wing. Two different theoretical formulations are presented and analysed for nonlinear behavior. The first formulation, which is more conventional, assumes zero equilibrias and...
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Format: | Others |
Language: | en_US |
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Texas A&M University
2006
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Online Access: | http://hdl.handle.net/1969.1/3846 |