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Dynamic Stability Analysis of Functionally Graded Plates Subjected to Complex Loads

机译:复合载荷功能梯度板的动态稳定性分析

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The paper investigates the dynamic stability of thick functionally graded plates subjected to aero-thermo-mechanical loads, using the moving least squares differential quadrature method. Temperature field is assumed to be a uniform distribution over the plate plane, and varied in the thickness direction only. Material properties are assumed to be temperature dependent and graded in the thickness direction in the simple power law manner. The equilibrium equations governing the dynamic stability of the plate are derived by the Hamilton's principle, then these equations are discretized by the moving least squares differential quadrature method. The boundaries of the instability region are obtained using the principle of Bolotin's method and are conveniently represented in the non-dimensional excitation frequency to load amplitude plane. The influence of various factors such as gradient index, temperature, mechanical and aerodynamic loads, thickness and aspect ratios, as well as the boundary conditions on the dynamic instability region are carefully studied.
机译:本文使用移动最小二乘差分法正交方法研究了经受航空热机械负荷的厚功能渐变平板的动态稳定性。假设温度场在板平面上是均匀的分布,并且仅在厚度方向上变化。假设材料特性以简单的功率法方式在厚度方向上依赖于温度和渐变。通过汉密尔顿的原理推导出板的动态稳定性的平衡方程,然后通过移动最小二乘差分正交方法离散化这些方程。使用Bolotin方法的原理获得不稳定区域的边界,并且在非维激励频率中方便地表示为负载幅度平面。仔细研究了各种因素,例如梯度指数,温度,机械和空气动力载荷,厚度和纵横比以及动态不稳定性区域的边界条件的影响。

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