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Nonlinear breathing vibrations of eccentric rotating composite laminated circular cylindrical shell subjected to temperature, rotating speed and external excitations

机译:非线性呼吸振动偏心旋转复合层叠圆柱形圆柱形壳体经受温度,旋转速度和外部激励

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In this paper, the nonlinear breathing vibrations of an eccentric rotating composite laminated circular cylindrical shell are studied for the first time, which is subjected to the lateral and temperature excitations. Based on Donnell thin shear deformation theory, von Korman-type nonlinear relation and Hamilton's principle, the nonlinear partial differential governing equations of motion are established for the eccentric rotating composite laminated circular cylindrical shell. The nonlinear partial differential governing equations of motion are discretized into a set of coupled nonlinear ordinary differential equations of motion by Galerkin approach. Based on the case of 1:2 internal resonance and principal parametric resonance-1/2 subharmonic resonance, the method of multiple scales is employed to obtain four-dimensional nonlinear averaged equations. Considering the effects of different parameters, for example, the eccentricity ratio, the geometric parameters and the excitations, the nonlinear dynamic behaviors and the jumping phenomena are exhibited for the frequency-response curves and the amplitude-response curves. The periodic and chaotic motions of the eccentric rotating composite laminated circular cylindrical shell are found when the rotating speed corresponds to the internal resonant point at the certain conditions for different lateral and temperature excitations. (C) 2019 Elsevier Ltd. All rights reserved.
机译:本文首次研究了偏心旋转复合叠层圆柱形壳体的非线性呼吸振动,其进行横向和温度激发。基于Donnell薄剪切变形理论,Von Korman型非线性关系和汉密尔顿原理,为偏心旋转复合层压圆柱形壳建立了运动的非线性偏差控制方程。通过Galerkin方法离散地分成运动的非线性部分差分管理方程被离散化为一组耦合的非线性常见常规方程。基于1:2内部共振和主参数共振-1 / 2次谐振谐振的情况,采用多种尺度的方法来获得四维非线性平均方程。考虑到不同参数的影响,例如,偏心比,几何参数和激发,非线性动态行为和跳跃现象被展示用于频率响应曲线和幅度响应曲线。当旋转速度对应于不同侧向和温度激发的某些条件下的内部谐振点时,发现偏心旋转复合叠层圆柱形壳体的周期性和混沌动作。 (c)2019 Elsevier Ltd.保留所有权利。

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