Dynamic response of thick laminated annular sector plates subjected to moving load

• Published in: Composite structures Vol. 92; no. 1; pp. 155 - 163
• Main Authors: Malekzadeh, P., Golbahar Haghighi, M.R., Gholami, M.
• Format: Journal Article
• Language: English
• Published: Kidlington Elsevier Ltd 2010; Elsevier
• Subjects: Differential quadrature; Exact sciences and technology; Fundamental areas of phenomenology (including applications); Laminated annular sector plates; Layerwise theory; Moving load; Physics; Solid mechanics; Static elasticity (thermoelasticity...); Structural and continuum mechanics; Three-dimensional elasticity; Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...); Laminated annular sector plates; Layerwise theory; Differential quadrature; Moving load; Three-dimensional elasticity; Distributed load; Curved beam; Annular plate; Stratified material; Vibration; Simple support; Thick plate; Modeling; Quadrature; Sector structure; Tridimensional elasticity; Convergence rate; Moving plate; Non linear effect; Differential method; Finite difference method
• ISSN: 0263-8223; 1879-1085
• DOI: 10.1016/j.compstruct.2009.07.020

The dynamic response of thick laminated annular sector plates with simply supported radial edges subjected to a radially distributed line load, which moves along the circumferential direction, is studied. A three-dimensional hybrid method composed of series solution, the layerwise theory and the differential quadrature method in conjunction with the finite difference method is employed. The fast rate of convergence and high accuracy of the method are demonstrated through different examples. Additionally, as a limit case, the out-of-plane dynamic responses of circular curved beams is obtained and compared with those of an unconstrained higher order shear deformation curved beam theory, which is formulated here. Then, the effects of different parameters such as the sector angle, thickness-to-outer radius ratio, ply lay out and the load velocity on the out-of-plane response of the symmetric and antisymmetric cross-ply laminated sector plates are investigated. The results can be used as benchmark solutions for future works.