ملخص البحث :
This paper presents a study of free vibration of perforated laminate composite plate. The modal
characteristics consist of three layers, the material is hard orthotropic composite material, with simply
support (SSSS), Clamped boundary (CCCC) and simple clamed conditions (SCSC) are applied at all four
edges of the plate.. The natural frequency and mode shape of the plates have been obtained using ANSYS
15. Eight-node isopaprametric layered shell elements (SHELL 281) are employed in the modeling for
describing the vibrations of these perforated laminate composite plates. The effect of number of holes, hole
area ratio, lamination angles and boundary condition on vibrations are investigated. The convergence study
was achieved for numerically and compare with present literature. The results showed that the frequencies
of the plate with one hole at the center are different from the perforated plate when maintaining a fixed
ratio hole area, as well the lamination angle has a clear effect on the increase and decrease of the
fundamental frequency for all the tested cases.
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سنة النشر : 2018
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تصنيف البحث : other
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