Stress in a Curved Skin Panel of a Pressurized Fuselage

Stress in a Curved Skin Panel of a Pressurized Fuselage The problem solved is that of an initially curved circumferential skin strip, representing a section of the panel midway between frames, continuous over the stringers which act as sinking supports and transfer part of the internal pressure load to the frames. The remainder of the pressure load produces hoop tension in the skin strip, but the maximum total stress including bending in the skin at the stringer, which is evaluated, is usually greater than would arise from hoop tension alone, in an unstiffened shell. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Stress in a Curved Skin Panel of a Pressurized Fuselage

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032852
Publisher site
See Article on Publisher Site

Abstract

The problem solved is that of an initially curved circumferential skin strip, representing a section of the panel midway between frames, continuous over the stringers which act as sinking supports and transfer part of the internal pressure load to the frames. The remainder of the pressure load produces hoop tension in the skin strip, but the maximum total stress including bending in the skin at the stringer, which is evaluated, is usually greater than would arise from hoop tension alone, in an unstiffened shell.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Jul 1, 1957

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