基于辛空间波的正交各向异性圆柱壳随机振动分析方法
收稿日期: 2025-05-30
修回日期: 2025-07-28
录用日期: 2025-08-11
网络出版日期: 2025-08-18
基金资助
强度与结构完整性全国重点实验室开放基金(ASSIKFJJ202303003);工业装备结构分析国家重点实验室开放基金(GZ23101)
A symplectic-wave-based method for random vibration analysis of orthotropic cylindrical shells
Received date: 2025-05-30
Revised date: 2025-07-28
Accepted date: 2025-08-11
Online published: 2025-08-18
Supported by
Open Project of the National Key Laboratory of Strength and Structural Integrity(ASSIKFJJ202303003);Optimization and CAE Software for Industrial Equipment(GZ23101);Open Project of the State Key Laboratory of Structural Analysis
针对湍流边界层作用下正交各向异性圆柱壳的随机振动问题,提出基于辛空间波的随机振动分析方法。首先,根据湍流边界层半经验模型,将湍流边界层作用下正交各向异性圆柱壳的随机振动响应转化为简谐位移求解;其次,基于Kirchhoff-Love薄壳理论,并结合Legendre变换,将Lagrange体系下轴压正交各向异性圆柱壳的弹性力学三大方程导入到Hamilton体系,形成统一的控制方程;然后利用辛空间内的波传播分析求解正交各向异性圆柱壳的简谐位移;最后,利用线性微分方程解的叠加原理将状态向量和激励力展开,得到解的周向叠加形式,再结合辛正交关系和一阶线性微分方程的求解方式,求解得到简谐位移。相比于模态叠加法,本方法能够解析地处理任意边界条件,且具有较高的收敛速度和计算精度。通过数值算例验证了本方法的收敛性和有效性,并分析了轴压变化对正交各向异性圆柱壳随机振动响应的影响。
米家琪 , 姜永平 , 高汝鑫 . 基于辛空间波的正交各向异性圆柱壳随机振动分析方法[J]. 航空学报, 2026 , 47(3) : 232322 -232322 . DOI: 10.7527/S1000-6893.2025.32322
A symplectic-wave-based method is proposed for the random vibration analysis of orthotropic cylindrical shells under turbulent boundary layer. Firstly, based on the semi-empirical model of turbulent boundary layer, the random vibration response of orthotropic cylindrical shells under turbulent boundary layer is transformed into harmonic response. Then, according to Kirchhoff-Love theory and Legendre transformation, the unified governing equation is obtained from the fundamental equations for orthotropic cylindrical shells under axial compression in the Lagrangian system transferring into the Hamiltonian system. And, the harmonic response of orthotropic cylindrical shells is solved through wave propagation analysis. Finally, both the state vector and excitation are expanded to obtain circumferential superposition form of the solution by applying the superposition principle of linear differential equation solutions. By combining symplectic orthogonality with the solution for first-order linear differential equations, the harmonic response is obtained. Compared with the modal superposition method, the proposed method can analytically handle arbitrary boundary conditions with higher convergence speed and computational accuracy. Numerical examples validate the convergence and effectiveness of the method, and the influence of axial compression variations on the random vibration response of orthotropic cylindrical shells is analyzed.
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