Buckling Analysis of Laminated Composite Plate with Different Boundary Conditions using modified Fourier series

  • Widad I. Majeed College of Engineering-University of Baghdad
  • Zainab Abdul Kareem Abed College of Engineering-University of Baghdad
Keywords: buckling load, Rayleigh-Ritz method, different edge conditions, and composite laminated plate.

Abstract

Buckling analysis of a laminated composite thin plate with different boundary conditions subjected to in-plane uniform load are studied depending on classical laminated plate theory; analytically using (Rayleigh-Ritz method). Equation of motion of the plates was derived using the principle of virtual work and solved using modified Fourier displacement function that satisfies general edge conditions. The eigenvalue problem generated by using Ritz method, the set of linear algebraic equations can be solved using MATLAB for symmetric and anti-symmetric, cross and angle-ply laminated plate considering some design parameters such as aspect ratios, number of layers, lamination type and orthotropic ratio. The results obtained gives good agreement with those published by other researchers.

 

Downloads

Download data is not yet available.
Published
2019-07-31
How to Cite
Majeed, W. and Abed, Z. (2019) “Buckling Analysis of Laminated Composite Plate with Different Boundary Conditions using modified Fourier series”, Journal of Engineering, 25(8), pp. 1-18. doi: 10.31026/j.eng.2019.08.1.

Most read articles by the same author(s)