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TwoSpar Wing Stress Analysis

TwoSpar Wing Stress Analysis IN an article in the June, 1941, number of AIRCRAFT ENGINEERING, the writer gave an approximate investigation into the stress analysis of a twospar skincovered wing, the basis of the method being the determination of the moments and shears induced in the spars by the skin covering. These moments and shears are then superimposed on the moments and shears which would occur in the spars were the skin covering to be removed, this latter loading system being statically determinate. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb030979
Publisher site
See Article on Publisher Site

Abstract

IN an article in the June, 1941, number of AIRCRAFT ENGINEERING, the writer gave an approximate investigation into the stress analysis of a twospar skincovered wing, the basis of the method being the determination of the moments and shears induced in the spars by the skin covering. These moments and shears are then superimposed on the moments and shears which would occur in the spars were the skin covering to be removed, this latter loading system being statically determinate.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Jan 1, 1943

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