Large-Deflection Theory for Plates With Small Initial Curvature Loaded in Edge Compression

John M. Coan

Journal of Applied Mechanics · 1951 · 140 citations · 0 references

Concepts

TL;DR

Typical test plates have stress‑free supported edges and uniformly displaced loaded edges, yet earlier analyses assumed straight, parallel supported edges, ignoring the influence of edge distortion on plate behavior and stress distribution. This study evaluates whether current methods for determining the true critical load from measured deflections and strains of a nominally flat, simply supported rectangular isotropic plate with small initial curvature are accurate. The authors adapt Levy’s solution of von Kármán’s large‑deflection equations to model the nonuniform edge displacements that arise with stress‑free supported edges. Experimental data largely support the predicted behavior, confirming the analysis.

Abstract

Abstract This investigation of the buckling of a simply supported, rectangular isotropic plate with small initial curvature was undertaken to evaluate current procedures for deducing the true (flat plate) critical load from the measured deflections and strains of a nominally flat plate. The boundary conditions are those that are usually met in test practice but which have not been satisfied by earlier studies, i.e., stress-free supported edges and uniformly displaced loaded edges. Previous solutions require a distribution of transverse stress along the supported edges sufficient to keep them straight and parallel at all times. However, in most test specimens, the freedom of the supported edges to distort in the plane of the plate measurably influences the behavior of the plate and the stress distribution within it. Levy’s solution of von Kármán’s “large deflection” equations is adapted by the author to yield the nonuniform edge displacements that are characteristic of stress-free supported edges. Limited experimental evidence tends to confirm the predictions of this analysis.