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Accurate buckling loads of thin rectangular plates under parabolic edge compressions by the differential quadrature method
Authors:Xinwei Wang   Xinfeng Wang  Xudong Shi
Affiliation:aCollege of Aerospace Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, People's Republic of China
Abstract:The buckling of thin rectangular plates with nonlinearly distributed loadings along two opposite plate edges is analyzed by using the differential quadrature (DQ) method. The problem is considerably more complicated since it requires that first the plane elasticity problem be solved to obtain the distribution of in-plane stresses, and then the buckling problem be solved. Thus, very few analytical solutions (the only one available in the literature is for rectangular plates with all edges simply supported) have been available in the literature thus far. Detailed formulations and solution procedures are given herein. Nine combinations of boundary conditions and various aspect ratios are considered. Comparisons are made with a few existing analytical and/or finite element data. It has been found that a fast convergent rate can be achieved by the DQ method with non-uniform grids and very accurate results are obtained for the first time. It has also been found that the DQ results, verified by the finite element method with NASTRAN, are not quite close to the newly reported analytical solution. A possible reason is given to explain the difference.
Keywords:Buckling   Differential quadrature method   Nonlinear distributed load   Rectangular plate
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