Abstract
In this paper, the investigation of the free and forced vibration response of the laminated composite plate is carried out. This analysis is based on the first-order shear deformation theory (FSDT) in conjunction with the finite element method. The steady-state response has been obtained in the time domain using the Newmark method. Free vibration responses of laminated composite plates obtained have been compared with the results available in the literature and by modeling in ANSYS showing excellent agreement. The parametric study has been accomplished to investigate the effect of geometric parameters thickness ratio, load amplitude, and damping factor on the free and forced vibration behavior of the laminated composite plate.
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Ahmad, N., Khan, A.H., Amir, M. (2022). Free and Forced Flexural Vibration Responses of the Laminated Composite Plates. In: Kumar, R., Chauhan, V.S., Talha, M., Pathak, H. (eds) Machines, Mechanism and Robotics. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-16-0550-5_169
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DOI: https://doi.org/10.1007/978-981-16-0550-5_169
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