Stressed‐Skin Wings in Pure Torsion: Simple Solutions for the Proportion of the Torque Resisted by Two Spars in Differential Bending
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1945
Abstract
BEING basically a strain energy problem, no quick method has so far been evolved—to the author's knowledge—for the determination of the relative distribution of the torque between the skin tube and the spars for other conditions than those in which the wing section and the applied torque is constant throughout the span.
Citation
Kittelsen, H.M.J. (1945), "Stressed‐Skin Wings in Pure Torsion: Simple Solutions for the Proportion of the Torque Resisted by Two Spars in Differential Bending", Aircraft Engineering and Aerospace Technology, Vol. 17 No. 4, pp. 94-100. https://doi.org/10.1108/eb031234
Publisher
:MCB UP Ltd
Copyright © 1945, MCB UP Limited