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The Elementary Theory of. StressedSkin Construction

The Elementary Theory of. StressedSkin Construction AIRCRAFT wings, tail planes, fuselages and control surfaces have to satisfy certain mandatory requirements of stiffness. These requirements arc designed to ensure the absence of aeroelastic troubles. They all take the form of a minimum specified limit to a stiffness, calculated or measured under the application of a definite force and constraint system. A stiffness may be defined as the ratio of a force to its corresponding displacement see 5.2 and so the calculation of stiffnesses reduces itself to a deflection problem1.1 2. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

The Elementary Theory of. StressedSkin Construction

Aircraft Engineering and Aerospace Technology , Volume 21 (8): 4 – Aug 1, 1949

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031794
Publisher site
See Article on Publisher Site

Abstract

AIRCRAFT wings, tail planes, fuselages and control surfaces have to satisfy certain mandatory requirements of stiffness. These requirements arc designed to ensure the absence of aeroelastic troubles. They all take the form of a minimum specified limit to a stiffness, calculated or measured under the application of a definite force and constraint system. A stiffness may be defined as the ratio of a force to its corresponding displacement see 5.2 and so the calculation of stiffnesses reduces itself to a deflection problem1.1 2.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Aug 1, 1949

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