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SemiCantilever Wings

SemiCantilever Wings IN the following, the free flexional oscillations of a monoplane's semicantilever wing are given, taking into consideration the inner and outer parts of the strut as two systems coupled by elasticity. The result, which is identical with coupled electrical circuits, has been checked by tests with a light aeroplane. 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/eb029987
Publisher site
See Article on Publisher Site

Abstract

IN the following, the free flexional oscillations of a monoplane's semicantilever wing are given, taking into consideration the inner and outer parts of the strut as two systems coupled by elasticity. The result, which is identical with coupled electrical circuits, has been checked by tests with a light aeroplane.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Nov 1, 1935

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