2022
DOI: 10.1007/s11071-022-07805-9
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Stability and nonlinear vibration of an axially moving plate interacting with magnetic field and subsonic airflow in a narrow gap

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Cited by 16 publications
(2 citation statements)
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“…The NES-giant magnetostrictive-piezoelectric also performs International Journal of Energy Research well in suppressing nonlinear aeroelastic response and harvesting energy [175]. NES-giant magnetostrictive-piezoelectric has also been applied to the subsonic aeroelastic system, where the energy harvesting performance of the system is affected by periodic motion and instability [176]. The proposed piezoelectric energy harvester consists of a partially covered piezoelectric cantilever beam, as shown in Figure 20; the electromechanical coupling distribution parameter model of the device was as follows [177]:…”
Section: Piezoelectric Energy Harvestermentioning
confidence: 99%
“…The NES-giant magnetostrictive-piezoelectric also performs International Journal of Energy Research well in suppressing nonlinear aeroelastic response and harvesting energy [175]. NES-giant magnetostrictive-piezoelectric has also been applied to the subsonic aeroelastic system, where the energy harvesting performance of the system is affected by periodic motion and instability [176]. The proposed piezoelectric energy harvester consists of a partially covered piezoelectric cantilever beam, as shown in Figure 20; the electromechanical coupling distribution parameter model of the device was as follows [177]:…”
Section: Piezoelectric Energy Harvestermentioning
confidence: 99%
“…The study of geometric nonlinear aeroelasticity differs from general aeroelasticity [1] from the theoretical aspects as follows: One is the structural geometric nonlinear theory, which mainly addresses the static and dynamic analysis of the structure under large deformation [2][3][4]; The other is the study of surface aerodynamic theory [5], which mainly addresses the boundary condition dependent deformation state aerodynamic calculation method under large deformation conditions of the structure [6]; The third is the study of the structural/aerodynamic interface coupling method [7,8], which mainly investigates the multidimensional interpolation problem applicable to large deformation in space. The problem of subsonic aeroelasticity of plates focuses on the fluid-structure coupling between the structure and the airflow [9,10]. The variety of parameters, such as mass, damping and stiffness of the structure under the action of subsonic airflow affects the critical instability and nonlinear vibration characteristics of the structure [2,11].…”
Section: Introductionmentioning
confidence: 99%