Buckling of Oblique Plates with Clamped Edges Under Uniform Shear

Author:

Wittrick W. H.

Abstract

SummaryIn a previous paper the author derived, by the Rayleigh-Ritz method, a determinantal equation for obtaining the critical magnitude of any uniform system of edge stress applied to a clamped oblique plate. In the present paper this equation is used to derive values for the buckling stresses of clamped oblique plates subjected to pure shear along and perpendicular to two edges of the plate.As would be expected, it is found that reversal of the direction of the shear produces a change in the critical value. The lower value occurs when the shear is tending to increase the obliquity of the plate and critical values corresponding to this direction are calculated for 45° oblique plates with side ratios varying between 3/5 and 5/3. The critical values obtained for the reverse direction were obviously very inaccurate, due to the inadequacy of the series which was used to represent the buckling mode. As yet no satisfactory method has been found for overcoming this difficulty.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference6 articles.

1. On the stability under shearing forces of a flat elastic strip

2. Anderson R. A. (1951). Charts giving Critical Compressive Stress of Continuous Flat Sheet divided into Parallelogram-Shaped Panels. N.A.C.A. T.N. 2392, July 1951.

3. Budiansky B. and Connor R. W. (1948). Buckling Stresses of Clamped Rectangular Flat Plates in Shear. N.A.C.A. T.N. 1559, 1948.

4. Eine Lösung für die Berechnung der biegsamen rechteckigen Platten

5. Buckling of Oblique Plates with Clamped Edges under Uniform Compression;Wittrick;Aeronautical Quarterly,1953

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