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The Quarterly Journal of Mechanics and Applied Mathematics 1983 36(2):207-221; doi:10.1093/qjmam/36.2.207
© 1983 by Oxford University Press
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FREE VIBRATIONS OF ANTISYMMETRIC ANGLE-PLY LAMINATED CIRCULAR CYLINDRICAL PANELS

KOSTAS P. SOLDATOS

( Department of Mechanics, University of Ioannina Ioannina, Greece )

For the free-vibration problem of a general anisotropic laminated circular cylindrical panel, the Donnell-type equations of motion are quoted and expressed in terms of the panel middle-surface displacement components. For the case of an antisymmetric angle-ply laminated panel subjected to S3 simply-supported edge boundary conditions, these equations are solved by employing the method of Galerkin. Numerical results are presented for a family of graphite-epoxy regular antisymmetric angle-ply laminated circular cylindrical panels. The results confirm the expectation that for such a type of laminated composite the effect of stretching-bending coupling rapidly dies out as the number of layers increases. However, the panel seems to present a rather anomalous dynamic behaviour dependent on the values of both its shallowness and lamination angles, on the stretching-bending coupling phenomenon as well as on the type of the boundary conditions.


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