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Dynamic instability of composite plates subjected to non-uniform in-plane loads

机译:承受非均匀平面载荷的复合材料板的动态不稳定性

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In this paper, the dynamic instability of a shear deformable composite plate subjected to periodic non-uniform in-plane loading is studied for four sets of boundary conditions. The static component and the dynamic component of the applied periodic in-plane loading are assumed to vary according to either parabolic or linear distributions. Initially, the plate membrane problem is solved using the Ritz method to evaluate the plate in-plane stress distributions within the prebuckling range due to the applied non-uniform in-plane edge loading. Subsequently using the evaluated stress distribution within the plate, the equations governing the plate instability boundaries are formulated via Hamiltons variational principle. Employing Galerkins method, these partial differential equations are reduced into a set of ordinary differential equations (Mathieu type of equations) describing the plate dynamic instability behaviour. Following Bolotins method, the instability regions are determined from the boundaries of instability, which represents the periodic solution of the differential equations with period T and 2T to the Mathieu equations. The instability regions are determined for uniform, linear and parabolic dynamic in-plane loads using first-order and second-order approximations. Numerical results are also presented to bring out the effects of span to thickness ratio, shear deformation, aspect ratio, boundary conditions and static load factor on the instability regions.
机译:在本文中,研究了四组边界条件下承受周期性非均匀面内载荷的可剪切变形复合材料板的动力不稳定性。假定所施加的周期性面内载荷的静态分量和动态分量根据抛物线分布或线性分布而变化。最初,由于使用了不均匀的平面内边缘载荷,使用Ritz方法解决了板膜问题,以评估预屈曲范围内的板内平面应力分布。随后,使用评估后的板内应力分布,通过汉密尔顿变分原理来制定控制板不稳定性边界的方程。使用Galerkins方法,将这些偏微分方程简化为一组描述板动态不稳定性行为的常微分方程(Mathieu型方程)。根据Bolotins方法,从不稳定性的边界确定不稳定性区域,这表示周期为T和2T的微分方程对Mathieu方程的周期解。使用一阶和二阶逼近确定不均匀区域的均匀,线性和抛物线动态平面载荷。还给出了数值结果,以指出跨度与厚度之比,剪切变形,纵横比,边界条件和静态载荷系数对不稳定性区域的影响。

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