2008
DOI: 10.1016/j.finel.2008.01.010
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The use of Timoshenko's exact solution for a cantilever beam in adaptive analysis

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Cited by 63 publications
(31 citation statements)
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“…For the FEM approximation for the displacement u of the 2D plane stress model, we use eight node quadrilateral elements, see, for example, the work of Fish and Belytschko . This choice was also used in the works of Labuschagne et al and Aguarde and Deeks, which consider similar problems to the one considered in this paper. For the FEM approximation of the variables ( v T , θ ) of the Timoshenko beam model, we employ the two node Timoshenko beam elements as shown in the work of Friedman and Kosmatka that provides a stiffness matrix, which is exactly integrated and is free of shear‐locking.…”
Section: Forward Problem and Damage Modelmentioning
confidence: 99%
“…For the FEM approximation for the displacement u of the 2D plane stress model, we use eight node quadrilateral elements, see, for example, the work of Fish and Belytschko . This choice was also used in the works of Labuschagne et al and Aguarde and Deeks, which consider similar problems to the one considered in this paper. For the FEM approximation of the variables ( v T , θ ) of the Timoshenko beam model, we employ the two node Timoshenko beam elements as shown in the work of Friedman and Kosmatka that provides a stiffness matrix, which is exactly integrated and is free of shear‐locking.…”
Section: Forward Problem and Damage Modelmentioning
confidence: 99%
“…The clamped cantilever beam is a standard benchmark for 2D elasticity, consisting of a rectangular beam, which is subject to Dirichlet boundary conditions at one end and to a shear load at the opposite one. Depending on how the boundary condition and the loading are defined, the obtained solution with exhibit a very different regularity . In order to produce a smooth solution, we here take the shear load g to be parabolic on the loaded edge and the essential boundary conditions along the clamped edge are applied according to the analytical solution given by Timoshenko and Goodier: ux=Py6ĒI()false(6L3xfalse)x+false(2+trueν¯false)y23D22false(1+trueν¯false), -5.3emuy=P6ĒI()3trueν¯y2false(Lxfalse)+false(3Lxfalse)x2, where Ē=Efalse/false(1ν2false), trueν¯=νfalse/false(1νfalse), and I is the second‐area moment of the beam section.…”
Section: Numerical Experimentsmentioning
confidence: 99%
“…We considered the indeterminate beam problem shown in Figure 3, which is a fixed end supported beam applied by a Dirac delta function [12,13]. The exact integration and reduced integration were used to analyze the problems.…”
Section: The Fixed End Supported Beam Applied By a Dirac Delta Functimentioning
confidence: 99%