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The Bending of Fuselage Shells

The Bending of Fuselage Shells THE paper suggests a new approach to the calculation of the bending strength of semimonocoque and possibly fully monocoque aircraft fuselage shells. The method described uses directly loaddeflexion graphs obtained from laboratory compression tests on panels representative of the shell at the section under consideration, and is analogous to the calculation of the form factor for a solid beam section, which factor is dependent on the shape of the section and on the stressstrain relationship of the material of which the beam is made. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

The Bending of Fuselage Shells

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031763
Publisher site
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Abstract

THE paper suggests a new approach to the calculation of the bending strength of semimonocoque and possibly fully monocoque aircraft fuselage shells. The method described uses directly loaddeflexion graphs obtained from laboratory compression tests on panels representative of the shell at the section under consideration, and is analogous to the calculation of the form factor for a solid beam section, which factor is dependent on the shape of the section and on the stressstrain relationship of the material of which the beam is made.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: May 1, 1949

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