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Volume 11, Issue 8
1 August 1939
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 11, Issue 8
Review Article| August 01 1939

Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening Available to Purchase

E.J. Richards, B.A., B.Sc.
E.J. Richards, B.A., B.Sc.
Mr. Richards is a member of the technical staff of The Bristol Aeroplane Co., Ltd.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1939
Aircraft Engineering (1939) 11 (8): 301–305.
https://doi.org/10.1108/eb030524

A GENERAL solution is obtained for the diffusion of stress in n equal and equally spaced stringers in a stiffened panel subject to any boundary conditions at the ends of the stringers.

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© MCB UP Limited
1939
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