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Analysis of dynamic stability for composite laminated cylindrical shells with delaminations

机译:复合材料层合圆柱壳脱层动力稳定性分析

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摘要

By introducing the Heaviside step function into the assumed displacement components and using the Rayleigh-Ritz method for minimizing the total potential energy, a set of dynamic governing equations for the delaminated cylindrical shells is derived. Then, the dynamic governing equations are written as the Mathieu-type equations to describe the parametric vibrating behavior of the shells, and these equations are solved by employing the Bolotin method. The numerical results for the dynamic stability of laminated cylindrical shells with delaminations are presented. The effects of the amplitude of external excitation, the delamination size and location and the material properties on the natural frequency and the principal dynamic instability region of the delaminated cylindrical shells are discussed. Present results are compared with available data.
机译:通过将Heaviside阶跃函数引入到假定的位移分量中,并使用Rayleigh-Ritz方法来最小化总势能,导出了一组用于分层圆柱壳的动态控制方程。然后,将动态控制方程写为Mathieu型方程来描述壳体的参数振动行为,并通过Bolotin方法求解这些方程。给出了分层的层合圆柱壳动力稳定性的数值结果。讨论了外部激励幅度,分层大小和位置以及材料特性对分层圆柱壳的固有频率和主要动态不稳定性区域的影响。将当前结果与可用数据进行比较。

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