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Some Structural Parameters for an AeroIsoclinic Wing

Some Structural Parameters for an AeroIsoclinic Wing The general theory of the clastic behaviour of a conventional singlecell wing stiffened with swept ribs or stringers has been dcvclopcd. It was shown that the swept members introduce a measure of skewness in the structural geometry of the wing which cause the wing to twist, as well as bend, under simple bending loads. This note shows that, if the sweepback angle is not more than 35 deg., it is possible to make a wing aeroisoclinic by introducing swept stringers. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Some Structural Parameters for an AeroIsoclinic Wing

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032202
Publisher site
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Abstract

The general theory of the clastic behaviour of a conventional singlecell wing stiffened with swept ribs or stringers has been dcvclopcd. It was shown that the swept members introduce a measure of skewness in the structural geometry of the wing which cause the wing to twist, as well as bend, under simple bending loads. This note shows that, if the sweepback angle is not more than 35 deg., it is possible to make a wing aeroisoclinic by introducing swept stringers.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Sep 1, 1952

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