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Nonlinear dynamic analysis of a double curvature honeycomb sandwich shell with simply supported boundaries by the homotopy analysis method

机译:用同伦分析法分析具有简单支撑边界的双曲蜂窝夹层壳的非线性动力学分析。

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Dynamics of a double curvature honeycomb sandwich shell with simply supported boundaries are studied in this paper. The nonlinear governing equations of the double curvature honeycomb sandwich shell subjected to transverse excitations are derived by using Hamilton's principle and Reddy's third-order shear deformation theory. Based on the homotopy analysis method, the average equations of the primary resonance and harmonic resonance are obtained. The influence of structural parameters, the transverse exciting force amplitude and transverse damping to the double curvature honeycomb sandwich shell are discussed by using the analytic approximation method. The amplitude-frequency response curves demonstrate softening nonlinearity in primary resonance (no internal resonance), hardening nonlinearity in 3 order superharmonic resonance and no jump phenomenon in 1/3 subharmonic resonance. The variation of nonlinear strength, multivalued jump point and multivalued region are detailed and discussed.
机译:研究了具有简单支撑边界的双曲率蜂窝夹层壳的动力学特性。利用汉密顿原理和雷迪三阶剪切变形理论,推导了双曲率蜂窝夹芯板在横向激励下的非线性控制方程。基于同伦分析方法,得到了一次共振和谐波共振的平均方程。利用解析逼近的方法,探讨了结构参数,横向激振力幅值和横向阻尼对双曲率蜂窝夹芯结构的影响。振幅-频率响应曲线显示出初级共振中的软化非线性(无内部共振),3阶超谐波共振中的非线性硬化和1/3次谐波中的无跳变现象。详细讨论了非线性强度,多值跳变点和多值区域的变化。

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