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  1. Axial-torsional buckling, single-flange, double-symmetry (+)
  2. Axial-torsional buckling, double-flange, double-symmetry (I)
  3. Axial-torsional buckling, single-flange, single-symmetry (T)
  4. Axial-torsional buckling, single-flange (L)
  • 0021 angle elastic, .

References  

Finite Rotations

Finite Rotations

This problem highlights the exceptional accuracy of the ExactFrame formulation for simulating large deformations

Pinched Shell Cylindrical Problem

Pinched Shell Cylindrical Problem

For ν=0.3\nu = 0.3 , R/t=100R/t = 100 , L/R=2L/R = 2 displacement under load is 164.24 P/(Et)164.24 \, P / (E t) . References Lindberg, G. M. M., D. Olson, and G. R. Cowper, “New Developments in the Finite Element Analysis of Shells”, Quarterly Bulletin of the Division of Mechanical Engineering and the National Aeronautical Establishment, National Research Council of Canada, vol. 4, 1969.

Pure flexure

Pure flexure

Bilinear quadrilateral elements are used to solve the infinitesimal pure bending problem.

Shell undergoing finite rotations

Shell

Shell undergoing finite rotations

Geometrically nonlinear analysis of a cantilever rolling up under the action of a point moment, performed with shell finite elements.

Transient response of a shallow spherical cap

Performance of continuum and shell elements for linear analysis of bending problems

Yacht Hull

http://130.149.89.49:2080/v2016/books/exa/default.htm?startat=ch01s01.html

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Benchmarks
Benchmarks
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