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Approximate Solution for Tapered Pin-Ended Struts

Published online by Cambridge University Press:  28 July 2016

Haydn Templeton
Haydn Templeton*
Affiliation:
Sir W. G. Armstrong Whitworth Aircraft, Ltd.
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Extract

Approximate solutions for the critical load of an axially loaded strut, and for the deflection produced in an eccentrically loaded strut, are obtained by the Energy Method. For most practical purposes these solutions compare favourably with solutions based on successive approximation, since for the same accuracy the time required for a solution by successive approximation is much greater.

Type
Research Article
Information
The Aeronautical Journal , Volume 48 , Issue 397 , January 1944 , pp. 6 - 11
Copyright
Copyright © Royal Aeronautical Society 1944

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References

* Taken from “ Determination of the Buckling Load of Struts with Successive Approximations ” by Dr. J. Ratzersdorfer. R.Ae.S. Journal, March, 1943.