Abstract
In this paper, the general equations of dynamic stability for composite laminated plates are derived by Hamilton principle. These general equations can be used to consider those different factors that affect the dynamic stability of laminated plates. The factors are transverse shear deformation, initial imperfections, longitudinal and rotational inertia, and ply-angle of the fiber, etc. The solutions of the fundamental equations show that some important characteristics of the dynamic instability can only be got by the consideration and analysis of those factors.
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Dedicated to the Tenth Anniversary and One Hundred Numbers of AMM (II)
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Cheng-ti, Z. Theory of nonlinear dynamic stability for composite laminated plates. Appl Math Mech 12, 113–120 (1991). https://doi.org/10.1007/BF02016530
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DOI: https://doi.org/10.1007/BF02016530