1980
DOI: 10.1016/0045-7949(80)90144-3
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A geometric and material nonlinear plate and shell element

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Cited by 218 publications
(45 citation statements)
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“…The strain tensor at any point in the element is, transverse shear strains where g', g', g' are the contravariant base vectors corresponding to the covariant base vectors g,, g,, gt, which are evaluated as given in equation (4). The appropriate interpolation of the in-layer strains and of the transverse shear strains to satisfy our shell element requirements as closely as possible is the key aspect of our element formulation.…”
Section: Higher-order Elements-an Eight-node Elementmentioning
confidence: 99%
See 1 more Smart Citation
“…The strain tensor at any point in the element is, transverse shear strains where g', g', g' are the contravariant base vectors corresponding to the covariant base vectors g,, g,, gt, which are evaluated as given in equation (4). The appropriate interpolation of the in-layer strains and of the transverse shear strains to satisfy our shell element requirements as closely as possible is the key aspect of our element formulation.…”
Section: Higher-order Elements-an Eight-node Elementmentioning
confidence: 99%
“…For the analytical patch test in bending we consider a single general quadrilateral flat element with nodal point co-ordinates xt, xk,, k = 1, 2, 3, 4 and constant thickness h. This is one of the elements shown in Figure 1. Our objective is to study analytically how this element behaves and whether when placed into the patch of Figure 1, the patch test is passed.…”
Section: [ + a R T T % L + A L -mentioning
confidence: 99%
“…The procedure to achieve the elastic and geometric stiffness matrices for the sixteen-node shell element is presented in Bathe and Bolourchi (1982).…”
Section: Nonlinear Finite Element Analysismentioning
confidence: 99%
“…1 gives an illustration of the element. The interpolation function used for the geometry is given by tX i-L1 (hk) (tX)+ n (hk) (a) tV97i (4) where tX k=global coordinate of node k, tXI global coordinate at a generic point on the shell, hk=shape function on r-s plane associated with node k, a=thickness of the shell, t Vn. component i of the unit normal vector, t j i to the mid-surface of the element at node Jg.…”
Section: Isoparametric Formulationmentioning
confidence: 99%