Nonlinear Dynamics of Thick Composite Laminated Plates Including the Effect of Transverse Shear and Rotary Inertia

Authors

  • Muhsin J. Jweeg Nahrain University, College of Engineering
  • Sameera A Abed Al-wahed University of Technology
  • Wafaa M. Salih University of Technology

Keywords:

Composite, Plate, Shear, Inertia

Abstract

In this work, a suggested analytical solution for nonlinear dynamic analysis of (fiber-reinforced) composite laminated thick plate is developed by using first-order

shear deformation theory (FSDT). A computer program was built for this purpose for antisymmetric cross-ply and angle-ply, simply supported thick

laminated plate and the developed equations are solved by using (MATLAB V.7) program. The finite-element solution is also adopted using (ANSYS V.8) package, to confirm the analytical results. The results presented show the effect of plate thickness-to-side ratio (h/a), aspect ratio (a/b), number of

layers (N), the degree of orthotropic ratio (E1/E2), fiber orientation, boundary conditions, lamination scheme, and the effect of shear deformation and rotary inertia on the

thick laminated plate.

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Published

05-03-2008

How to Cite

[1]
M. J. Jweeg, S. A. Abed Al-wahed, and W. M. Salih, “Nonlinear Dynamics of Thick Composite Laminated Plates Including the Effect of Transverse Shear and Rotary Inertia”, NUCEJ, vol. 11, no. 2, pp. 251–262, Mar. 2008, Accessed: Dec. 23, 2024. [Online]. Available: https://oldjournal.eng.nahrainuniv.edu.iq/index.php/main/article/view/518

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