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

Learn More →

Variation in Strength of Nominally Identical Tail Planes

Variation in Strength of Nominally Identical Tail Planes IN the strength testing of major components of aircraft structures, considerations of time and expense do not usually permit the use of more than one specimen of any component. However, it has long been realized that, if a number of nominally identical specimens of any given component were tested, there would be some variation in failing load and probably in mode of failure, and that this variation would depend on the type of construction. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Variation in Strength of Nominally Identical Tail Planes

Download PDF
3 pages

Loading next page...
 
/lp/emerald-publishing/variation-in-strength-of-nominally-identical-tail-planes-iO5KKtonFK
Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032188
Publisher site
See Article on Publisher Site

Abstract

IN the strength testing of major components of aircraft structures, considerations of time and expense do not usually permit the use of more than one specimen of any component. However, it has long been realized that, if a number of nominally identical specimens of any given component were tested, there would be some variation in failing load and probably in mode of failure, and that this variation would depend on the type of construction.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Aug 1, 1952

There are no references for this article.