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Tapered Spar Frames: An Approximate Method for the Determination of the Stresses in, and Deflections of, a Fuselage

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 April 1941

Abstract

THE methods and formula outlined below are applicable to any shape of fuselage, but an elliptical one is assumed to serve as an illustration.

Citation

Kittelsen, H.M.J. (1941), "Tapered Spar Frames: An Approximate Method for the Determination of the Stresses in, and Deflections of, a Fuselage", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 4, pp. 90-94. https://doi.org/10.1108/eb030756

Publisher

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MCB UP Ltd

Copyright © 1941, MCB UP Limited