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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:双曲率蜂窝夹层壳的非线性动力学分析,具有统一分析法的支持边界

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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:本文研究了具有简单支持的边界的双曲率蜂窝夹层壳的动态。通过使用Hamilton的原理和Reddy的三阶剪切变形理论来源经受横向激发的双曲率蜂窝夹层壳的非线性控制方程。基于同型分析方法,获得了初级谐振和谐振谐振的平均方程。通过使用分析近似法讨论了结构参数,横向激发力幅度和横向阻尼到双曲率蜂窝夹层壳的影响。幅度响应曲线在初级谐振(无内部共振)中展示软化非线性,3个阶超声共振中的硬化非线性,并且在1/3次谐振共振中没有跳跃现象。非线性强度,多值跳跃点和多价区域的变化是详细的和讨论的。

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