A Suggested Analytical Solution For Laminated Closed Cylindrical Shells Using General Third Shell Theory (G.T.T.)

Authors

  • Muhsin J. Jweeg Engineering Mechanic Departmaent Nahrain University
  • Wedad I. Alazzawy Engineering Mechanic Departmaent nahrain University

Keywords:

Laminate, Cylindrical, Shells

Abstract

Transient solutions will be developed for laminated simply supported closed cylindrical shells subjected to a uniform dynamic pressure at the outer surface of the cylinder. These solutions are obtained by using General Third Shell Theory (G.T.T.). Rectangular pulse, triangular pulse, sinusoidal ulse and (ramp-constant) load-time varying functions are studied and the required equilibrium equations are developed. The central deformation and principle stresses are investigated for different cross-ply laminates.

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Published

03-03-2007

Issue

Vol. 10 No. 1 (2007): Nahrain University, College of Engineering Journal (NUCEJ)

Section

Articles

License

The authors retain the copyright of their manuscript by submitting the work to this journal, and all open access articles are distributed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International (CC-BY-NC 4.0), which permits use for any non-commercial purpose, distribution, and reproduction in any medium, provided that the original work is properly cited.

How to Cite

[1]
M. J. Jweeg and W. I. Alazzawy, “A Suggested Analytical Solution For Laminated Closed Cylindrical Shells Using General Third Shell Theory (G.T.T.)”, NUCEJ, vol. 10, no. 1, pp. 11–26, Mar. 2007, Accessed: Dec. 23, 2024. [Online]. Available: https://oldjournal.eng.nahrainuniv.edu.iq/index.php/main/article/view/483