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Volume 13, Issue 4
1 April 1941
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 13, Issue 4
Review Article| April 01 1941

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

Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1941
Aircraft Engineering (1941) 13 (4): 90–94.
https://doi.org/10.1108/eb030756

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

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© MCB UP Limited
1941
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