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NASA NTRS · 19900035958

Finite element mesh refinement criteria for stress analysis

Abstract

This paper discusses procedures for finite-element mesh selection and refinement. The objective is to improve accuracy. The procedures are based on (1) the minimization of the stiffness matrix race (optimizing node location); (2) the use of h-version refinement (rezoning, element size reduction, and increasing the number of elements); and (3) the use of p-version refinement (increasing the order of polynomial approximation of the elements). A step-by-step procedure of mesh selection, improvement, and refinement is presented. The criteria for 'goodness' of a mesh are based on strain energy, displacement, and stress values at selected critical points of a structure. An analysis of an aircraft lug problem is presented as an example.

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BibTeXRIS

Kittur, Madan G., Huston, Ronald L.. 1990-01-01. Finite element mesh refinement criteria for stress analysis. https://ntrs.nasa.gov/citations/19900035958

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