Works cited by this work

29 works

Work: Computational Experiments to Evaluate the Approaches to the Modeling of Viscoelastic Plates Motion Based on Various Theories

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2. Numerical Analysis of the Nonlinear Flutter of Viscoelastic Plates

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3. On certain methods of solving systems of integrodifferential equations encountered in viscoelasticity problems

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4. Numerical investigation of nonlinear vibrations of viscoelastic plates and cylindrical panels in a gas flow

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   ArticleVibration and Dynamic AnalysisJournal of Applied Mechanics and Technical Physics200719 citations

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7. Nonlinear flutter of viscoelastic rectangular plates and cylindrical panels of a composite with a concentrated masses

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8. Numerical study of the dependence of the critical flutter speed and time of a plate on rheological parameters

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9. Nonconservative stability of viscoelastic rectangular plates with free edges under uniformly distributed follower force

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10. Flutter of a viscoelastic plate

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11. Nonlinear vibrations of plates in axial pulsating flow

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12. Nonlinear LCO “amplitude–frequency” characteristics for plates fluttering at supersonic speeds

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14. Dynamic stability of a completely free plate subjected to a controlled non-conservative follower force

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15. Coherent structures and their influence on the dynamics of aeroelastic panels

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16. Active aeroelastic flutter analysis and vibration control of supersonic beams using the piezoelectric actuator/sensor pairs

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17. An electret-based aeroelastic flutter energy harvester

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18. Supersonic flutter suppression of electrorheological fluid-based adaptive panels resting on elastic foundations using sliding mode control

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19. Flutter of Finite-Span Flexible Plates in Uniform Flow

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21. Non-linear vibrations and stability of a periodically supported rectangular plate in axial flow

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22. Æolian tones and stall flutter of lengthy objects in fluid flows

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23. Aeroelastic flutter energy harvester design: the sensitivity of the driving instability to system parameters

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24. Optimal locations of piezoelectric patches for supersonic flutter control of honeycomb sandwich panels, using the NSGA-II method

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