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Large Deflection Effects in Antisymmetric Cross-Ply Laminated Strips and Plates

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Composite Structures
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Abstract

A finite difference Dynamic Relaxation (DR) computer program has been developed for large deflection Mindlin plate analysis. The program has been used to obtain solutions for an antisymmetric cross-ply laminated strip subjected to uniform lateral pressure and different edge conditions. It is demonstrated that the bending stiffness of a strip with simply supported in- plane fixed edges is dependent on the direction of the applied load. It is also established that only under simply supported in-plane fixed edge conditions does the flexural stiffness of a strip or a rectangular plate with antisymmetric cross-ply lay-up depend on the direction of the applied pressure. Moreover, it is shown that the directional behaviour is due to the B1 1 stiffness which arises in the expressions for the stress resultant, Nx, and the stress couple, Mx. The Bl1 term undergoes a sign change as the direction of bending changes.

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References

  1. Sun, C. T. and Chin, H., On large deflection effects in unsymmetric cross-ply composite laminates. J. Comp. Mater., 22 (11) (1988) 1045–59.

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  2. Turvey, G. J. and Osman, M. Y., Elastic large deflection analysis of isotropic rectangular Mindlin plates. Int. J. Mech. Sci., 22 (1990) 1–14.

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  3. Turvey, G. J. and Osman, M. Y., Large deflection analysis of orthotropic Mindlin plates. Proceedings of the 12th Energy-Resources Technology Conference and Exhibition, Houston, Texas, 1989, pp. 163–72.

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© 1991 Elsevier Science Publishers LTD.

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Turvey, G.J., Osman, M.Y. (1991). Large Deflection Effects in Antisymmetric Cross-Ply Laminated Strips and Plates. In: Marshall, I.H. (eds) Composite Structures. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-3662-4_31

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  • DOI: https://doi.org/10.1007/978-94-011-3662-4_31

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-1-85166-647-8

  • Online ISBN: 978-94-011-3662-4

  • eBook Packages: Springer Book Archive

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