Stability of discretely stringer-stiffened cylindrical shells.

descriptionPublicationkeyboard_double_arrow_right Article 01 Jun 1973 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:AIAA Journal, volume 11, pages 810-814 (issn: 0001-1452, eissn: 1533-385X,

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Authors: Wang, James Ting-Shun; Lin, Yu-Jyi;

doi: 10.2514/3.6836

Stability of discretely stringer-stiffened cylindrical shells.

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Abstract

The paper presents and analysis for the stability characteristics of axially compressed simply supported thin cylindrical shells stiffened by longitudinal stringers. Stringers and panels between stringers are treated as discrete structural components. Donnell's shell theory is used for panels, and each stringer is governed by a set of four ordinary differential equations.

Related Organizations

University of Kentucky
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Georgia Institute of Technology
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Keywords

Membranes, Bifurcation and buckling, Shells

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