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Flutter Control of a Lifting Surface via Visco-Hysteretic Vibration Absorbers

  • Lacarbonara, Walter ;
  • Cetraro, Marek
  • Received : 2011.10.10
  • Accepted : 2011.11.29
  • Published : 2011.12.30

Abstract

In this paper, a visco-hysteretic vibration absorber (VA) is proposed to increase the flutter speed of an airfoil and enhance damping in the pre- and post-flutter regimes. The passive system consists of a parallel arrangement of a dashpot and a rateindependent hysteretic element, represented by the Bouc-Wen differential model. The equations of motion are obtained and various tools of linear and nonlinear dynamics are employed to study the effects of the visco-hysteretic VA in the pre- and postflutter ranges.

Keywords

Visco-hysteretic vibration absorber;Flutter control

References

  1. Behal, A., Marzocca, P., Rao, V. M., and Gnann, A. (2006). Nonlinear adaptive control of an aeroelastic two-dimensional lifting surface. Journal of Guidance, Control, and Dynamics, 29, 382-390. https://doi.org/10.2514/1.14011
  2. Bouc, R. (1967). Forced vibrations of mechanical systems with hysteresis. Proceedings of the 4th International Conference on Nonlinear Oscillations, Prague, Czechoslovakia.
  3. Carpineto, N., Lacarbonara, W., and Vestroni, F. (2010). Hysteresis-based nonlinear vibration absorbers. Proceedings of the 13th Conference on Nonlinear Vibrations, Dynamics Eurodyn, and Mulitbody Systems, Blacksburg, VA.
  4. Carpineto, N., Vestroni, F., and Lacarbonara, W. (2011). Vibration mitigation by means of hysteretic tuned mass dampers. Proceedings of the 8th International Conference on Structural Dynamics, Leuven, Belgium.
  5. Den Hartog, J. P. (1934). Mechanical Vibrations. New York: McGraw-Hill.
  6. Frahm, H. (1911). Device for Damping Vibration of Bodies. US Patent No. 989958.
  7. Glauert, H. (1947). The Elements of Aerofoil and Airscrew Theory. 2nd ed. New York: Cambridge University Press.
  8. Hu, J. L. and Zhou, L. (2007). Semi-active flutter control of a high-aspect-ratio wing using multiple MR dampers. Proceedings of the Conference on Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems, San Diego, CA.
  9. Lacarbonara, W. and Vestroni, F. (2003). Nonclassical responses of oscillators with hysteresis. Nonlinear Dynamics, 32, 235-258. https://doi.org/10.1023/A:1024423626386
  10. Lee, Y. S., Kerschen, G., Michael McFarland, D., Joel Hill, W., Nichkawde, C., Strganac, T. W., Bergman, L. A., and Vakakis, A. F. (2007a). Suppressing aeroelastic instability using broadband passive targeted energy transfers, part 2: experiments. AIAA Journal, 45, 2391-2400.
  11. Lee, Y. S., Vakakis, A. F., Bergman, L. A., McFarland, D. M., and Kerschen, G. (2007b). Suppressing aeroelastic instability using broadband passive targeted energy transfers, part 1: theory. AIAA Journal, 45, 693-711. https://doi.org/10.2514/1.24062
  12. Marzocca, P., Librescu, L., and Silva, W. A. (2002). Flutter, postflutter, and control of a supersonic wing section. Journal of Guidance, Control, and Dynamics, 25, 962-970. https://doi.org/10.2514/2.4970
  13. McGowan, A. M. R. (1999). Feasibility study on using shunted piezoelectrics to reduce aeroelastic response. Proceedings of SPIE, 3674, 178-195.
  14. Meirovitch, L. (1970). Methods of Analytical Dynamics. New York: McGraw-Hill.
  15. Njuguna, J. (2007). Flutter prediction, suppression and control in aircraft composite wings as a design prerequisite: A survey. Structural Control and Health Monitoring, 14, 715-758. https://doi.org/10.1002/stc.170
  16. Reed, W. H., Cazier, F. W., and Foughner, J. T. (1980). Passive Control of Wing/Store Flutter. NASA Technical Memorandum 81865. Washington, DC: National Aeronautics and Space Administration.
  17. Richard, R. E. and Clark, R. L. (2003). Delta wing flutter control using spatially optimized transducers. Journal of Intelligent Material Systems and Structures, 14, 677-691. https://doi.org/10.1177/1045389X03038584
  18. Rocha, J., Moniz, P., and Suleman, A. (2007). Aeroelastic control of a wing with active skins using piezoelectric patches. Mechanics of Advanced Materials and Structures, 14, 23-32. https://doi.org/10.1080/15376490600864505
  19. Schweiger, J., Simpson, J., Weiss, F., Coetzee, E., and Boller, C. (1999). Needs for the analysis and integrated design optimization of active and passive structure for active aeroelastic wings. Proceedings of SPIE, 3668, 117-130.
  20. Vestroni, F., Lacarbonara, W., and Carpineto, N. (2011). Hysteretic Tuned Mass Damper for Passive Control of Mechanical Vibrations. Italy Patent No. RM2011A000434.
  21. Wen, Y. K. (1976). Method for random vibration of hysteretic systems. Journal of the Engineering Mechanics-ASCE, 102, 249-263.

Cited by

  1. Flutter Control of a Two-Degrees-of-Freedom Airfoil Using a Nonlinear Tuned Vibration Absorber vol.12, pp.5, 2017, https://doi.org/10.1115/1.4036420
  2. A fully passive nonlinear piezoelectric vibration absorber vol.376, pp.2127, 2018, https://doi.org/10.1098/rsta.2017.0142