Nonlinear Vibration Analysis for Stiffened Cylindrical Shells Subjected to Electromagnetic Environment

• Published in: Shock and vibration 2021, Vol.2021 (1)
• Main Authors: Li, Xue-Qin, Bai, Guang-Chen, Song, Lu-Kai, Zhang, Wei
• Format: Article
• Language: English
• Subjects: Accuracy; Analysis; Aspect ratio; Behavior; Cylindrical shells; Differential equations; Differential geometry; Electromagnetism; Engineering; Equations of motion; Excitation; Frequency ranges; Geometric nonlinearity; Hamilton's principle; Investigations; Liu, Timothy; Mathematical analysis; Multiscale analysis; Nonlinear differential equations; Nonlinear dynamics; Partial differential equations; Perturbation methods; Resonance; Shear deformation; Shells; Vibration; Vibration analysis; Vibration tests
• ISSN: 1070-9622; 1875-9203
• DOI: 10.1155/2021/9983459

The nonlinear vibration behaviors of stiffened cylindrical shells under electromagnetic excitations, transverse excitations, and in-plane excitations are studied for the first time in this paper. Given the first-order shear deformation theory and Hamilton principle, the nonlinear partial differential governing equations of motion are derived with considering the von Karman geometric nonlinearity. By employing the Galerkin discretization procedure, the partial differential equations are diverted to a set of coupled nonlinear ordinary differential equations of motion. Based on the case of 1 : 2 internal resonance and principal resonance-1/2 subharmonic parametric resonance, the multiscale method of perturbation analysis is employed to precisely acquire the four-dimensional nonlinear averaged equations. From the resonant response analysis and nonlinear dynamic simulation, we discovered that the unstable regions of stiffened cylindrical shells can be narrowed by decreasing the external excitation or increasing the magnetic intensity, and their working frequency range can be expanded by reducing the in-plane excitation. Moreover, the different nonlinear dynamic responses of the stiffened cylindrical shell are acquired by controlling stiffener number, stiffener size, and aspect ratio. The presented approach in this paper can provide an efficient analytical framework for nonlinear dynamics theories of stiffened cylindrical shells and will shed light on complex structure design in vibration test engineering.