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Tapered Beams: Suggested Solutions for Some Typical Aircraft Cases

E.H. Atkin, B.Sc. (Design staff of Boulton, Paul Aircraft, Ltd., Wolverhampton)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 December 1938

Abstract

PART III.—Taper Beams with uniform thin webs and concentrated booms of constant cross‐sectional area. This type of girder is shown in Fig. 1.

Citation

Atkin, E.H. (1938), "Tapered Beams: Suggested Solutions for Some Typical Aircraft Cases", Aircraft Engineering and Aerospace Technology, Vol. 10 No. 12, pp. 371-374. https://doi.org/10.1108/eb030409

Publisher

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MCB UP Ltd

Copyright © 1938, MCB UP Limited