Computational modeling of coupled membrane-beam flexible wings for micro air vehicles
暂无分享,去创建一个
Raymond E. Gordnier | Peter J. Attar | Padmanabhan Seshaiyer | Lauren A. Ferguson | P. Seshaiyer | R. Gordnier | Lauren Ferguson
[1] Padmanabhan Seshaiyer,et al. Stability and convergence of nonconforming hp finite-element methods☆ , 2003 .
[2] Philip Smith,et al. A non-conforming finite element method for sub-meshing , 2003, Appl. Math. Comput..
[3] Peter Ifju,et al. Flexible-wing-based Micro Air Vehicles , 2002 .
[4] Padmanabhan Seshaiyer,et al. hp submeshing via non-conforming finite element methods , 2000 .
[5] Wei Shyy,et al. Flapping and flexible wings for biological and micro air vehicles , 1999 .
[6] J. Humphrey,et al. Finite element analysis of nonlinear orthotropic hyperelastic membranes , 1996 .
[7] R. Taylor,et al. Theory and finite element formulation of rubberlike membrane shells using principal stretches , 1992 .
[8] Wei H. Yang,et al. General Deformations of Neo-Hookean Membranes , 1973 .
[9] A. Spencer,et al. The Static Theory of Finite Elasticity , 1970 .
[10] J. T. Oden,et al. Finite strains and displacements of elastic membranes by the finite element method , 1967 .