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The Quadrilateral Shear Panel

The Quadrilateral Shear Panel Among the problems introduced by swept wings is that of the nonrectangular panel in equilibrium under loading applied tangentially along its edges. The present article examines the state of stress in a general uniform quadrilateral panel and, for the benefit of stiffness calculations, the strain energy stored in it. Stable conditions are assumed. The problem of replacing such a panel by diamond bracing is also treated. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

The Quadrilateral Shear Panel

Garvey, S.J.
Aircraft Engineering and Aerospace Technology , Volume 23 (5): 11 – May 1, 1951
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032029
Publisher site
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Abstract

Among the problems introduced by swept wings is that of the nonrectangular panel in equilibrium under loading applied tangentially along its edges. The present article examines the state of stress in a general uniform quadrilateral panel and, for the benefit of stiffness calculations, the strain energy stored in it. Stable conditions are assumed. The problem of replacing such a panel by diamond bracing is also treated.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: May 1, 1951

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