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A Solution to the Problem of Torsion‐Flexure: A Method of Using the Principle of Least Work and Calculus of Variations to Establish the Potential Energy Integrals

R.L. Mordellet (Stress analyst, Ateliers d'Aviation L. Breguet.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1950

36

Abstract

FOR the past fifteen years nearly all aircraft structures have been of the shell or stressed‐skin type and problems pertaining to this type of structure have been steadily tackled and finally solved for practical use by the designers.

Citation

Mordellet, R.L. (1950), "A Solution to the Problem of Torsion‐Flexure: A Method of Using the Principle of Least Work and Calculus of Variations to Establish the Potential Energy Integrals", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 11, pp. 335-337. https://doi.org/10.1108/eb031965

Publisher

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MCB UP Ltd

Copyright © 1950, MCB UP Limited

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