Get 20M+ Full-Text Papers For Less Than $1.50/day. Start a 14-Day Trial for You or Your Team.

Learn More →

Stress Diffusion Problems

Stress Diffusion Problems THE case now to be considered is shown diagrammatically in FIG. 12, which also gives the additional notation required. The problem is to determine how a bending moment, applied at one end to the longerons only, is diffused into the whole section, being finally distributed according to the usual beam theory of bending. The differential equation to be satisfied by the displacement w is equation B2, and if we take the origin at the centre we may take sR, hr, xR sin and yR cos . Equation B2 then becomes http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Stress Diffusion Problems

Goodey, W.J.
Aircraft Engineering and Aerospace Technology , Volume 18 (9): 4 – Sep 1, 1946
Download PDF
4 pages

Loading next page...
 
/lp/emerald-publishing/stress-diffusion-problems-juoPDxfNsH

References

References for this paper are not available at this time. We will be adding them shortly, thank you for your patience.

Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031418
Publisher site
See Article on Publisher Site

Abstract

THE case now to be considered is shown diagrammatically in FIG. 12, which also gives the additional notation required. The problem is to determine how a bending moment, applied at one end to the longerons only, is diffused into the whole section, being finally distributed according to the usual beam theory of bending. The differential equation to be satisfied by the displacement w is equation B2, and if we take the origin at the centre we may take sR, hr, xR sin and yR cos . Equation B2 then becomes

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Sep 1, 1946

There are no references for this article.