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NASA NTRS · 19750019357

A triangular thin shell finite element: Linear analysis

Abstract

The formulation of the linear stiffness matrix for a doubly-curved triangular thin shell element, using a modified potential energy principle, is described. The strain energy component of the potential energy is expressed in terms of displacements and displacement gradients by use of consistent Koiter strain-displacement equations. The element inplane and normal displacement fields are approximated by complete cubic polynomials. The interelement displacement admissibility conditions are met in the global representation by imposition of constraint conditions on the interelement boundaries; the constraints represent the modification of the potential energy. Errors due to the nonzero strains under rigid body motion are shown to be of small importance for practical grid refinements through performance of extensive comparison analyses.

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BibTeXRIS

Thomas, G. R., Gallagher, R. H.. 1975-07-01. A triangular thin shell finite element: Linear analysis. https://ntrs.nasa.gov/citations/19750019357

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