Built‐in and Continuous Beams

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 November 1942

Abstract

PROBLEMS relating to built‐in or rigid‐end members under transverse loading are frequently encountered by the aircraft engineer. In the following paper discussion of relevant theorems leads to the development of Clapeyron's Theorem of Three Moments. The latter is particularly valuable in, for example, estimating the crankshaft bearing loads in a non‐radial engine. Attention is also drawn to Wilson's method of solving continuous beam problems. This simple method produces results identical with those given by the Theorem of Three Moments and deserves wider recognition.

Citation

Dudley, L. (1942), "Built‐in and Continuous Beams", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 11, pp. 306-319. https://doi.org/10.1108/eb030957

Download as .RIS

Publisher

:

MCB UP Ltd

Copyright © 1942, MCB UP Limited

Please note you might not have access to this content

You may be able to access this content by login via Shibboleth, Open Athens or with your Emerald account.
If you would like to contact us about accessing this content, click the button and fill out the form.
To rent this content from Deepdyve, please click the button.