2021
DOI: 10.1016/j.apm.2020.12.001
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Large deformation analysis of fully incompressible hyperelastic curved beams

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Cited by 12 publications
(6 citation statements)
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“…Recent studies have examined the performance of the developed elements under large rotations by solving this problem using meshes ranging from three up to a hundred of elements. 18,19 The exact solution to this problem is a circular arc with radius R = EI∕M. To deform the rod into a full closed circle, an end moment M = 2𝜋EI∕L needs to be applied.…”
Section: Pure Bending Of a Cantilever Beammentioning
confidence: 99%
See 1 more Smart Citation
“…Recent studies have examined the performance of the developed elements under large rotations by solving this problem using meshes ranging from three up to a hundred of elements. 18,19 The exact solution to this problem is a circular arc with radius R = EI∕M. To deform the rod into a full closed circle, an end moment M = 2𝜋EI∕L needs to be applied.…”
Section: Pure Bending Of a Cantilever Beammentioning
confidence: 99%
“…The first test, serving as a benchmark, deals with a cantilever of length L and bending stiffness EI loaded by a concentrated end moment M on its right end. Recent studies have examined the performance of the developed elements under large rotations by solving this problem using meshes ranging from three up to a hundred of elements 18,19 . The exact solution to this problem is a circular arc with radius R=EI/M.…”
Section: Numerical Examplesmentioning
confidence: 99%
“…The beam has a length of 4 meters, and the bending stiffness EI of the beam cross-section is assumed to be l. The bending moments applied on the right end are up to 4π, which can make the member wind twice around itself. This is a classical nonlinear structural analysis problem that has been investigated by several researchers [71][72][73][74] during the past decades. Recent studies tried to solve this large-rotation problem using the fine-meshed FEM, where the number of which ranges from three up to a hundred for a single member [71][72], showing the intensive computational expense.…”
Section: Example 1 -Cantilever Beams Under End Momentmentioning
confidence: 99%
“…Perform the linearlization procedure to Eqs. ( 6) and ( 7), two non-linear parts for finite deformation analysis are derived (10) where K tan is the tangent stiffness matrix that includes the geometric non-linear and material nonlinear parts of the problem…”
Section: Three-dimensional Finite Element Formulations For Non-linear...mentioning
confidence: 99%