Flexure‐Torsion Failure of Panels
- 1 July 1954
- journal article
- Published by Emerald Publishing in Aircraft Engineering and Aerospace Technology
- Vol. 26 (7) , 213-219
- https://doi.org/10.1108/eb032442
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:Keywords
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