A Variational Principle for Reconstruction of Elastic Deformations in Shear Deformable Plates and Shells
暂无分享,去创建一个
[1] T. Hughes,et al. A three-node mindlin plate element with improved transverse shear , 1985 .
[2] Peter Lancaster,et al. Curve and surface fitting - an introduction , 1986 .
[3] Erdogan Madenci,et al. Nonlinear analysis of laminates through a mindlin-type shear deformable shallow shell element , 1997 .
[4] Nicholas Zabaras,et al. Investigation of regularization parameters and error estimating in inverse elasticity problems , 1994 .
[5] E. Reissner. ON THE THEORY OF BENDING OF ELASTIC PLATES , 1944 .
[6] E. Reissner. The effect of transverse shear deformation on the bending of elastic plates , 1945 .
[7] H. R. Riggs,et al. A Novel Four-Node Quadrilateral Smoothing Element for Stress Enhancement and Error Estimation , 1998 .
[8] Martin A. Putnam,et al. Determination of cantilever plate shapes using wavelength division multiplexed fiber Bragg grating sensors and a least-squares strain-fitting algorithm , 1998 .
[9] H. Ronald Riggs,et al. An improved variational method for finite element stress recovery and a posteriori error estimation , 1998 .
[10] A. N. Tikhonov,et al. Solutions of ill-posed problems , 1977 .
[11] Fu-Kuo Chang,et al. Structural Health Monitoring , 2016 .
[12] E. Reissner,et al. Reflections on the Theory of Elastic Plates , 1985 .
[13] E. Haugse,et al. Structural Shape Identification from Experimental Strains Using a Modal Transformation Technique , 2003 .
[14] Kim Stelson,et al. Finite Element Analysis of Some Inverse Elasticity Problems , 1989 .
[15] Pei-Ling Liu,et al. Direct identification of non-uniform beams using static strains , 1996 .
[16] A. Tessler,et al. A C o -anisoparametric three-node shallow shell element , 1990 .
[17] D. Schnur,et al. Finite element solution of two‐dimensional inverse elastic problems using spatial smoothing , 1990 .
[18] Alexander Tessler,et al. An Inverse Interpolation Method Utilizing In-Flight Strain Measurements for Determining Loads and Structural Response of Aerospace Vehicles , 2001 .