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Rectangular Plates with Stiffeners: The Buckling of Simply Supported Plates under Compressive Stress

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 September 1942

Abstract

The Differential Equation of the Problem and the Solution. A RECTANGULAR plate of length a with simply supported edges is reinforced by equal longitudinal ribs at equal distances b and is submitted to the action of uniformly distributed compressive forces N along the x‐axis (Fig. 1). For every strip b we have the differential equation for the deflection w

Citation

Ratzersdorfer, J. (1942), "Rectangular Plates with Stiffeners: The Buckling of Simply Supported Plates under Compressive Stress", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 9, pp. 260-264. https://doi.org/10.1108/eb030942

Publisher

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MCB UP Ltd

Copyright © 1942, MCB UP Limited