Vibration suppression on the composite laminated plates subjected to aerodynamic and harmonic excitations based on the nonlinear piezoelectric shunt damping
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Publication:6072750
DOI10.1016/J.APM.2023.04.026zbMath1525.74136OpenAlexW4366978405MaRDI QIDQ6072750
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Publication date: 13 October 2023
Published in: Applied Mathematical Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.apm.2023.04.026
aerodynamic pressureplate structurescomplexification-averaging methodnegative capacitancenonlinear piezoelectric shunt damping
Cites Work
- Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap
- Nonlinear aero-thermal flutter postponement of supersonic laminated composite beams with shape memory alloys
- Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material
- On the dynamic response regimes of a viscoelastic isolation system integrated with a nonlinear energy sink
- Panel flutter analysis of cracked functionally graded plates in yawed supersonic flow with thermal effects
- Board multimodal vibration control using piezoelectric synchronized switch damping techniques
- The Rayleigh–Ritz Method for Structural Analysis
- A fully passive nonlinear piezoelectric vibration absorber
- The suppression of nonlinear panel flutter response at elevated temperatures using a nonlinear energy sink
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