TY - JOUR
T1 - Random vibro-acoustic analysis of thick laminated cylindrical shells under turbulent boundary layer via symplectic wave-based method
AU - Mi, Jiaqi
AU - Jiang, Yongping
AU - Gao, Ruxin
AU - Li, Yuanyuan
N1 - Publisher Copyright:
© 2025 Elsevier Inc.
PY - 2025/12
Y1 - 2025/12
N2 - The symplectic wave-based method is developed for the random vibro-acoustic analysis of laminated cylindrical shells under turbulent boundary layer. First, based on the semi-empirical model of the turbulent boundary layer, the random vibration response of laminated cylindrical shells under turbulent boundary layer is transformed into the superposition of a series of steady-state response. Secondly, the governing equations for the vibration analysis of laminated cylindrical shells in the Hamiltonian system are established based on the first-order shear deformation theory, and the steady-state response of the laminated cylindrical shell is solved using wave propagation analysis in the symplectic system. Finally, the sound pressure spectrum inside the cylindrical shell cavity is obtained from the vibration response of the laminated cylindrical shell structure according to the Kirchhoff-Helmholtz integral. Compared to the modal decomposition 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 proposed method, and the influence of axial pressure on the random vibro-acoustic response of laminated cylindrical shells is analyzed.
AB - The symplectic wave-based method is developed for the random vibro-acoustic analysis of laminated cylindrical shells under turbulent boundary layer. First, based on the semi-empirical model of the turbulent boundary layer, the random vibration response of laminated cylindrical shells under turbulent boundary layer is transformed into the superposition of a series of steady-state response. Secondly, the governing equations for the vibration analysis of laminated cylindrical shells in the Hamiltonian system are established based on the first-order shear deformation theory, and the steady-state response of the laminated cylindrical shell is solved using wave propagation analysis in the symplectic system. Finally, the sound pressure spectrum inside the cylindrical shell cavity is obtained from the vibration response of the laminated cylindrical shell structure according to the Kirchhoff-Helmholtz integral. Compared to the modal decomposition 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 proposed method, and the influence of axial pressure on the random vibro-acoustic response of laminated cylindrical shells is analyzed.
KW - Arbitrary boundary conditions
KW - Axial pressure
KW - Symplectic system
KW - Thick laminated cylindrical shells
KW - Turbulent boundary layer
UR - http://www.scopus.com/inward/record.url?scp=105008204006&partnerID=8YFLogxK
U2 - 10.1016/j.apm.2025.116252
DO - 10.1016/j.apm.2025.116252
M3 - Article
AN - SCOPUS:105008204006
SN - 0307-904X
VL - 148
JO - Applied Mathematical Modelling
JF - Applied Mathematical Modelling
M1 - 116252
ER -