Stiffness of Thin Shells: Brief Notes on the Optimum Stiffness Obtainable for a Given Weight of Material
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 September 1936
Abstract
IN these notes, the stillness of thin shells is discussed from three different viewpoints. Throughout, the basis of the argument is the elementary Batho‐Bredt torsion formula and no attempt is made to discuss the effects of end or other constraints on the straight‐forward conclusions obtained on this simple basis.
Citation
Roxbee Cox, H. (1936), "Stiffness of Thin Shells: Brief Notes on the Optimum Stiffness Obtainable for a Given Weight of Material", Aircraft Engineering and Aerospace Technology, Vol. 8 No. 9, pp. 245-246. https://doi.org/10.1108/eb030091
Publisher
:MCB UP Ltd
Copyright © 1936, MCB UP Limited