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NASA NTRS · 19750019358

A triangular thin shell finite element: Nonlinear analysis

Abstract

Aspects of the formulation of a triangular thin shell finite element which pertain to geometrically nonlinear (small strain, finite displacement) behavior are described. The procedure for solution of the resulting nonlinear algebraic equations combines a one-step incremental (tangent stiffness) approach with one iteration in the Newton-Raphson mode. A method is presented which permits a rational estimation of step size in this procedure. Limit points are calculated by means of a superposition scheme coupled to the incremental side of the solution procedure while bifurcation points are calculated through a process of interpolation of the determinants of the tangent-stiffness matrix. Numerical results are obtained for a flat plate and two curved shell problems and are compared with alternative solutions.

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BibTeXRIS

Thomas, G. R., Gallagher, R. H.. 1975-07-01. A triangular thin shell finite element: Nonlinear analysis. https://ntrs.nasa.gov/citations/19750019358

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