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Professor Ali Reza Setoodeh

Mechanical and Aerospace Engineering
Shiraz University of Technology, Iran

Selected Publications (For more see the link Prof. Ali Reza Setoodeh):
A. R. Setoodeh, G. Karami, A solution for the vibration and buckling of composite laminates with elastically restrained edges, Composite Structure 60 (2003) 245-253
A.R. Setoodeh, G. Karami, Static, free vibration and buckling analysis of anisotropic thick laminated composite plates on distributed and point elastic supports using a 3-D layer-wise FEM, Eng. Struct., 26 (2004), pp. 211-220
Malekzadeh P, Setoodeh A (2007) Large deformation analysis of moderately thick laminated plates on nonlinear elastic foundations by DQM. Comput Struct 80(4):569–579
P. Malekzadeh, A. R. Setoodeh, and E. Barmshouri, “A hybrid layerwise and differential quadrature method for in-plane free vibration of laminated thick circular arches,” J. Sound Vibr., 315, 212–225 (2008).
Setoodeh A.R., Attariani H., Khosrownejad M.: Nickel nanowires under uniaxial loads: a molecular dynamics simulation study. Comput. Mater. Sci. 44, 378–384 (2008)
Setoodeh, A.R., Jahanshahi, M. and Attariani, H. (2009), "Atomistic simulations of the buckling behavior of perfect and defective silicon carbide nanotubes", Comput. Mater. Sci., 47(2), 388-397.
Setoodeh AR, Malekzadeh P, Vosoughi AR (2011) Nonlinear free vibration of orthotropic graphene sheets using nonlocal Mindlin plate theory. Proc Inst Mech Eng Part C J Mech Eng Sci 1–11. doi: 10.1177/0954406211428997
Malekzadeh P., Setoodeh A.R., Alibeygi Beni A.: Small scale effect on the free vibration of orthotropic arbitrary straight-sided quadrilateral nanoplates. Compos. Struct. 93, 1631–1639 (2011)
Malekzadeh, P., Setoodeh, A.R., Alibeygi Beni, A.: Small scale effect on the thermal buckling of orthotropic arbitrary straight-sided quadrilateral nanoplates embedded in an elastic medium. Compos. Struct. 93, 2083–2089 (2011)
A. R. Setoodeh, M. Tahani, and E. Selahi, “Hybrid layerwise-differential quadrature transient dynamic analysis of functionally graded axisymmetric cylindrical shells subjected to dynamic pressure,” Compos. Struct., 93, 2663-2670 (2011).

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