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TECHNICAL PAPERS

Elasticity Solutions for Laminated Orthotropic Cylindrical Shells Subjected to Localized Longitudinal and Circumferential Moments

[+] Author and Article Information
K. Bhaskar

Department of Aerospace Engineering, Indian Institute of Technology, Madras, Chennai 600 036, India

N. Ganapathysaran

Tata Consultancy Services, Chennai, India

J. Pressure Vessel Technol 125(1), 26-35 (Jan 31, 2003) (10 pages) doi:10.1115/1.1511519 History: Received August 14, 2001; Revised July 30, 2002; Online January 31, 2003
Copyright © 2003 by ASME
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References

Figures

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Shell geometry and coordinates
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Loading—(a) longitudinal moment, (b) circumferential moment
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Variation of ur for the case of the longitudinal moment—(a) longitudinal, (b) circumferential
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Variation of σz for the case of the longitudinal moment—(a) longitudinal, (b) circumferential
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Variation of σθ for the case of the longitudinal moment—(a) longitudinal (b) circumferential
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Thicknesswise variation of uz for the case of circumferential moment—(a) at the center of the patch, (b) away from the patch
Grahic Jump Location
Variation of ur for the case of the circumferential moment—(a) longitudinal, (b) circumferential
Grahic Jump Location
Variation of σz for the case of the circumferential moment—(a) longitudinal, (b) circumferential
Grahic Jump Location
Variation of σθ for the case of the circumferential moment—(a) longitudinal, (b) circumferential
Grahic Jump Location
Thickness-wise variation of uz for the case of circumferential moment—(a) at the center of the patch, (b) away from the patch

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