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Parametric and internal resonance of a transporting plate with a varying tension
- Source :
- Nonlinear Dynamics. 98:2491-2508
- Publication Year :
- 2019
- Publisher :
- Springer Science and Business Media LLC, 2019.
-
Abstract
- Nonlinear transverse vibrations of in-plane accelerating viscoelastic plates are analytically and numerically investigated in the presence of principal parametric and 3:1 internal resonance. Due to the axial acceleration, the plate tension varies in the transporting direction. For a range of mean velocity, the natural frequency of the second mode is almost equal to three times that of the first mode, and that leads to a possible 3:1 internal resonance. The governing equation and the corresponding boundary conditions are derived from the generalized Hamilton principle. The method of multiple scales is applied to reveal that the steady-state responses have two types: trivial and nontrivial (two-mode) solutions. The stabilities of the steady-state responses are determined via the Routh–Hurwitz criterion. The analytical investigations demonstrate the effects of viscous damping coefficient, the viscoelastic coefficient, and the moving speed fluctuation amplitude on the stability of zero solutions and the amplitude of the nontrivial solutions. A differential quadrature scheme is developed to solve numerically the governing equation under the given boundary conditions. The numerical results agree well with the approximate analytical results.
- Subjects :
- Physics
Applied Mathematics
Mechanical Engineering
Mathematical analysis
Aerospace Engineering
Ocean Engineering
Natural frequency
01 natural sciences
Quadrature (mathematics)
Vibration
Nonlinear system
symbols.namesake
Amplitude
Control and Systems Engineering
0103 physical sciences
symbols
Hamilton's principle
Boundary value problem
Electrical and Electronic Engineering
010301 acoustics
Multiple-scale analysis
Subjects
Details
- ISSN :
- 1573269X and 0924090X
- Volume :
- 98
- Database :
- OpenAIRE
- Journal :
- Nonlinear Dynamics
- Accession number :
- edsair.doi...........9b90d536efd36ccaad28cd734f406079
- Full Text :
- https://doi.org/10.1007/s11071-019-04981-z