Response of Laminated Composite Cylindrical Shell Using Higher Order Shear Deformation Theory-Reference-Cited by-同舟云学术

Response of Laminated Composite Cylindrical Shell Using Higher Order Shear Deformation Theory

Published:2019-07-01 Issue:1 Volume:1240 Page:012006
ISSN:1742-6588
Container-title:Journal of Physics: Conference Series
language:
Short-container-title:J. Phys.: Conf. Ser.

Author:

Suryawanshi Aniket A,Gadade Appaso M

Abstract

Abstract The present work proposes the response of composite laminated cylindrical shell using higher order shear deformation theory (HSDT). For the finite element formulation a displacement field having five degrees of freedom is considered and a nine noded isoparametric element is used. The finite element model is developed using MATLAB code. The numerical results are obtained for the deflection of cylindrical shell for arbitrary boundary condition, stacking angle and radius to thickness ratio. The results are validated using literature and it shows good agreement

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Link

https://iopscience.iop.org/article/10.1088/1742-6596/1240/1/012006/pdf

Reference11 articles.

1. On the small free vibrations and deformations of the elastic shells;Love;Phil. Trans. Roy. Sot.(London), Ser. A,1888

2. A consistent first approximation in the general theory of thin elastic shells;Koiter,1959

3. Note on the foundations of the theory of small displacements of orthotropic shells;Hildebrand;National Advisory Comm. Aeru. Tech. Notes, No.,1949

4. Stress-strain relations in the theory of thin elastic shells;Reissner;J. Muth. Phys.,1952

5. Effects of anisotropy in axisymmetric cylindrical shells;Gulati;Journal of Applied Mechanics,1967

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