ACTA AERONAUTICAET ASTRONAUTICA SINICA >
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
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.
Jiaqi MI , Yongping JIANG , Ruxin GAO . A symplectic-wave-based method for random vibration analysis of orthotropic cylindrical shells[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2026 , 47(3) : 232322 -232322 . DOI: 10.7527/S1000-6893.2025.32322
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