Response of moderately thick laminated composite plates on elastic foundation subjected to moving load

2013 ◽  
Vol 97 ◽  
pp. 286-295 ◽  
Author(s):  
A.R. Vosoughi ◽  
P. Malekzadeh ◽  
H. Razi
Author(s):  
M. T. Ahmadian ◽  
T. Pirbodaghi

In this paper, free vibration analysis of laminated composite plates is carried out using first shear deformation theory and finite element method. Effect of axial tension and compression forces on the natural frequencies of the structure is investigated. Applying elastic foundation under the laminated composite plates has enabled us to achieve desired frequencies. The displacements are based C° – nine plate bending element and each node has three degree of freedom. The equations of motion are derived using Hamilton's principle. Results indicate the tension forces will increase the natural frequency while the compression force reduces the natural frequency. The buckling force of plate is computed by increasing the absolute value of compressive force until the natural frequency tends to zero. Dynamic of moving mass in a circular path on the laminated composite plate is also investigated. Displacement of plate center reveals a sinusoidal pattern in time.


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