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Flexure‐Torsion Failure of Panels: A Study of Instability and Failure of Stiffened Panels under Compression when Buckling in Long Wavelengths

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1954

Abstract

The methods developed in sections (5)–(7) are now applied to the determination of the torsional cum flexural failing stresses in two panels. The following points should be noted:

Citation

Argyris, J.H. (1954), "Flexure‐Torsion Failure of Panels: A Study of Instability and Failure of Stiffened Panels under Compression when Buckling in Long Wavelengths", Aircraft Engineering and Aerospace Technology, Vol. 26 No. 7, pp. 213-219. https://doi.org/10.1108/eb032442

Publisher

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MCB UP Ltd

Copyright © 1954, MCB UP Limited