Structural Considerations of Filament Wound Cylindrical Shells. Report no. 6804

Wong, H.Y. (1968) Structural Considerations of Filament Wound Cylindrical Shells. Report no. 6804. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

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Abstract

The structural response of filament-wound cylindrical shells to a combination of applied loadings is investigated. In many cases the membrane theory forms an adequate basis for the analysis. By suitable arrangement of the filament orientations and layer thicknesses, an efficient structure can be achieved. Numerical examples are given to show their influence on the stress components. The strength of the shells can be judged according to some criterion. In the Appendix, the determination of the elastic constants is given.

Item Type:Research Reports or Papers (Technical Report)
Additional Information:University of Glasgow author: H.Y. Wong.
Status:Published
Glasgow Author(s) Enlighten ID:UNSPECIFIED
Authors: Wong, H.Y.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Publisher:Department of Aeronautics and Fluid Mechanics, University of Glasgow
Copyright Holders:Copyright © 1968 Department of Aeronautics and Fluid Mechanics, University of Glasgow
Publisher Policy:Reproduced with the permission of the Department

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