journal article·2003-10

An Approach for Finite Strains and Rotations of Shells of Revolution with Application to a Spherical Shell Under a Uniformly Distributed Pressure

Ayse Erdölen, R. Faruk Yükseler

Journal of Elastomers & Plastics· Volume 35· Issue 4
Publisher page

Abstract

A theoretical and numerical analysis of rubber-like shells of revolution undergoing finite strains and finite rotations with the application to the problem of a spherical shell subject to a uniformly distributed internal pressure is presented. The comparison of the results corresponding to two different definitions proposed for the reference surface of deformed rubber-like shells, an asymptotical solution, and the membrane solution is presented, as well.
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Research context

OpenAlex topics: Elasticity and Wave Propagation · Structural Analysis and Optimization · Advanced Theoretical and Applied Studies in Material Sciences and Geometry

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Affiliations

Department of Civil Engineering Yildiz Technical University Besiktas, Turkey,

Department of Civil Engineering Yildiz Technical University Besiktas, Turkey

References (11)

Show source-provided references
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4. 4. Koçak, A.E. and Yükseler, R.F. (1999). Finite Axisymmetric Strains and Rotations of Shells of Revolution with Application to the Problem of a Spherical Shell under a Point Load , Sixth Annual International Conference on Composites Engineering, Florida, pp. 421-422 .
5. 5. Koçak, A.E. and Yükseler, R.F. (2000). Nonlinear Analysis of Rubber-Like Shells of Revolution with to a Spherical Shell with Ring Loads, Bridging Large Spans , IASS-MSU Int. Sym., Turkey, pp. 357-364 .
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9. 9. Yükseler, R.F. The Parameters Affecting the Differences Between the Solutions Corresponding to Two Different Definitions of the Reference Surface of Deformed Rubber-Like Shells of Revolution , International Journal of Non-Linear Mechanics, to appear.
10. 10. Parnell, T.K. (1984). Numerical Improvement of Asymptotic Solutions and Nonlinear Shell Analysis, Ph.D. Thesis, Stanford University.
11. 10.1115/1.342284310.1115/1.3422843 ↗