The Stresses in a Circular Fuselage

Author:

Goodey W. J.

Abstract

The following investigations were made primarily in order to determine the manner of transmission of concentrated loads from the frames to the skin of a circular fuselage. The usual assumption, that the shear distribution in the skin adjacent to the frame is given by the simple “ beam theory,” was considered to be of doubtful validity, and for some time past the writer had suspected that a critical examination of the problem would show a very considerable variation from the ordinary theory in the immediate vicinity of the loaded frame. The writer's attention was first drawn to the problem by the work of Wignot, Combs and Ensrud in N.A.C.A. Technical Note No. 929, and the present investigations were made because a more fundamental approach to the subject was considered to be desirable.

Publisher

Cambridge University Press (CUP)

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The Stress Analysis of the Circular Conical Fuselage with Flexible Frames;The Journal of the Royal Aeronautical Society;1955-08

2. Bending Moments in Fuselage Frames Obtained by the Photoelastic Method;The Journal of the Royal Aeronautical Society;1953-11

3. Stress Analysis of Circular Frames in a Non-tapering Fuselage;The Journal of the Royal Aeronautical Society;1953-03

4. Shear Stress Concentration and Moment Reduction Factors for Reinforced Monocoque Cylinders Subjected to Concentrated Radial Loads;Journal of the Aeronautical Sciences;1949-05

5. Publication/Subscription/Member Data;Journal of the Aeronautical Sciences;1949-05

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