摘要
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.
| 投稿的翻译标题 | 基 于 辛 空 间 波 的 正 交 各 向 异 性 圆 柱 壳 随 机 振 动分 析 方 法 |
|---|---|
| 源语言 | 英语 |
| 文章编号 | 232322 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 47 |
| 期 | 3 |
| DOI | |
| 出版状态 | 已出版 - 2026 |
| 已对外发布 | 是 |
学术指纹
探究 '基 于 辛 空 间 波 的 正 交 各 向 异 性 圆 柱 壳 随 机 振 动分 析 方 法' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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