The Triangular Equilibrium Element in the Solution of Plate Bending Problems
- 1 May 1968
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 19 (2), 149-169
- https://doi.org/10.1017/s0001925900004546
Abstract
Summary: Further details are given of a recently developed triangular equilibrium element which is then applied, in conjunction with the complementary energy principle, to the finite element analysis of some plate bending problems. The element is demonstrated to have a straightforward and satisfactory application and to possess advantages over the conventional triangular displacement element.This publication has 3 references indexed in Scilit:
- A Triangular Equilibrium Element with Linearly Varying Bending Moments for Plate Bending ProblemsJournal of the Royal Aeronautical Society, 1967
- On Assumed Displacements for the Rectangular Plate Bending ElementJournal of the Royal Aeronautical Society, 1967
- Reinforced Fields of Triangular Elements with Linearly Varying Strain; Effect of Initial StrainsJournal of the Royal Aeronautical Society, 1965