Natural and forced vibrations of solid bodies with account for damping and prestressed state induced by piezoelectric elements
DOI:
https://doi.org/10.7242/1999-6691/2025.18.4.29Keywords:
natural and forced vibration, electro-viscoelasticity, prestress, viscous and Rayleigh damping, finite element methodAbstract
The widespread use of thin-walled structures subjected to undesirable dynamic phenomena necessitates the development of effective methods for controlling their vibrational characteristics to prevent resonance. A promising approach to solving this problem is the application of smart materials, particularly, piezoelectric elements, enabling the implementation of passive, active, and hybrid damping systems. This work investigates the natural and forced vibrations of piecewise-homogeneous electro-elastic and electro-viscoelastic bodies using the finite element method. A distinctive feature of the study is the consideration of the prestressed and predeformed state caused by an embedded piezoelectric element as a result of the reverse piezoelectric effect due to DC voltage supply. A mathematical formulation of the problem, interpreting the prestress state in terms of geometric stiffness, and accounting for viscous and Rayleigh damping mechanisms is developed based on the principle of virtual displacements. Using a plate with an embedded piezoelectric element as an example, the influence of the control voltage and the type of damping on the complex natural frequencies and amplitude-frequency responses is studied. It has been established that both viscous and Rayleigh damping have slight effect on the shift of resonant frequencies caused by the prestressed state. The results of solution of the forced vibration problem allow us to quantify a decrease in the vibration amplitude of the plate in the prestressed state caused by the piezoelectric element in the case of external excitation with frequency corresponding to the resonance frequency of the unloaded plate. The results presented demonstrate the influence of the prestressed state on the amplitude-frequency response of a plate with closely spaced natural frequencies at different values of the electric potential on the piezoelectric element.
Downloads
References
Dowell E.H. Aeroelasticity of plates and shells. Springer, 1975. 152 p.
Chai Y., Gao W., Ankay B., Li F., Zhang C. Aeroelastic analysis and flutter control of wings and panels: A review. International Journal of Mechanical System Dynamics. 2021. Vol. 1, no. 1. P. 5–34. DOI: 10.1002/msd2.12015
Muc A., Flis J., Augustyn M. Optimal Design of Plated/Shell Structures under Flutter Constraints—A Literature Review. Materials. 2019. Vol. 12, no. 24. 4215. DOI: 10.3390/ma12244215
Yao D., Zhang J., Lei J., Zhao Z., Zhang Y., Zhao Y., Pang J., Li J. A comprehensive review of acoustic metamaterials: Applications and challenges for lightweight noise control in large-scale transportation. Materials & Design. 2025. Vol. 260. 115002. DOI: 10.1016/j.matdes.2025.115002
Song G., Sethi V., Li H.-N. Vibration control of civil structures using piezoceramic smart materials: A review. Engineering Structures. 2006. Vol. 28, no. 11. P. 1513–1524. DOI: 10.1016/j.engstruct.2006.02.002
Yan-ting A., Ce Y., Liang W., Jing T. The influence of stiffened ribs on vibration of a thin-walled casing. 2017 9th International Conference on Modelling, Identification and Control (ICMIC). 2017. P. 60–64. DOI: 10.1109/ICMIC.2017.8321531
Najmi J., Khan H.A., Javaid S.S., Hameed A., Siddiqui F. Aeroelastic tailoring for aerospace applications. Heliyon. 2024. Vol. 10, no. 2. e24151. DOI: 10.1016/j.heliyon.2024.e24151
Ren R., Ma X., Yue H., Yang F., Lu Y. Stiffness enhancement methods for thin-walled aircraft structures: A review. Thin-Walled Structures. 2024. Vol. 201. 111995. DOI: 10.1016/j.tws.2024.111995
Forward R.L. Electronic damping of vibrations in optical structures. Applied Optics. 1979. Vol. 18, no. 5. P. 690–697. DOI: 10.1364/AO.18.000690
Hagood N.W., Flotow A. von. Damping of structural vibrations with piezoelectric materials and passive electrical networks. Journal of Sound and Vibration. 1991. Vol. 146, no. 2. P. 243–268. DOI: 10.1016/0022-460X(91)90762-9
Cobb R., Browning J., Canfield R., Miller S. F-16 Ventral Fin Buffet Alleviation Using Piezoelectric Actuators. 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2009. DOI: 10.2514/6.2009-2538
Abramovich H. Intelligent materials and structures. Walter de Gruyter, 2016. 378 p.
Hofmann V., Twiefel J. Self-Sensing with loaded piezoelectric Bending actuators. Sensors and Actuators A: Physical. 2017. Vol. 263. P. 737–743. DOI: 10.1016/j.sna.2017.06.004
Shivashankar P., Gopalakrishnan S. Review on the use of piezoelectric materials for active vibration, noise, and flow control. Smart Materials and Structures. 2020. Vol. 29, no. 5. 053001. DOI: 10.1088/1361-665X/ab7541
Vol’mir A.S. Nonlinear Dynamics of Plates and Shells [in Russian]. Moscow: Nauka, 1972. 432 p.
Kamenskikh A., Lekomtsev S., Matveenko V. Free Vibration of Prestressed Plates and Shallow Shells with Piezoelectric Elements. International Journal of Applied Mechanics. 2024. Vol. 16, no. 07. 2450072. DOI: 10.1142/S1758825124500728
Hernandes J.A., Almeida S.F.M., Nabarrete A. Stiffening effects on the free vibration behavior of composite plates with PZT actuators. Composite Structures. 2000. Vol. 49, no. 1. P. 55–63. DOI: 10.1016/S0263-8223(99)00125-7
Donadon M.V., Almeida S.F.M., Faria A.R. de. Stiffening effects on the natural frequencies of laminated plates with piezoelectric actuators. Composites Part B: Engineering. 2002. Vol. 33, no. 5. P. 335–342. DOI: 10.1016/s1359-8368(02)00026-4
Kasem M.M., Dowell E.H. A study of the natural modes of vibration and aeroelastic stability of a plate with a piezoelectric material. Smart Materials and Structures. 2018. Vol. 27, no. 7. 075043. DOI: 10.1088/1361-665X/aac8a7
Kasem M.M., Negm H., Elsabbagh A. Aeroelastic Modeling of Smart Composite Wings Using Geometric Stiffness. Journal of Aerospace Engineering. 2019. Vol. 32, no. 2. 04018143. DOI: 10.1061/(ASCE)AS.1943-5525.0000957
Salmani H., Bodo E., Hanke U., Vogl A., Jain S., Merlo S., Halvorsen E. Modal analysis of piezoelectrically actuated plates with built-in stress by computationally augmented interferometric experiments. Sensors and Actuators A: Physical. 2022. Vol. 337. 113444. DOI: 10.1016/j.sna.2022.113444
Abramovich H. Axial Stiffness Variation of Thin Walled Laminated Composite Beams Using Piezoelectric Patches- a New Experimental Insight. International Journal of Aeronautical Science & Aerospace Research. 2016. P. 97–105. DOI: 10.19070/2470-4415-1600012
Fridman Y., Abramovich H. Enhanced structural behavior of flexible laminated composite beams. Composite Structures. 2008. Vol. 82, no. 1. P. 140–154. DOI: 10.1016/j.compstruct.2007.05.007
Kuliński K., Przybylski J. Stability and vibrations control of a stepped beam using piezoelectric actuation. MATEC Web of Conferences. 2018. Vol. 157. 08004. DOI: 10.1051/matecconf/201815708004
Kuo S.- Y. Stiffening Effects on the Natural Frequencies of Laminated Beams with Piezoelectric Actuators. Journal of Aeronautics, Astronautics and Aviation, Series A. 2010. Vol. 42, no. 1. P. 67–72.
Zenz G., Humer A. Stability enhancement of beam-type structures by piezoelectric transducers: theoretical, numerical and experimental investigations. Acta Mechanica. 2015. Vol. 226, no. 12. P. 3961–3976. DOI: 10.1007/s00707-015-1445-9
Versiani T.d.S.S., Tsunematsu D.Q., Donadon M.V., Silvestre F.J., Guimarães Neto A.B., Guimarães A. Aeroelastic behavior of a composite plate-like wing under piezoelectrically induced stresses. Mechanical Systems and Signal Processing. 2020. Vol. 143. 106795. DOI: 10.1016/j.ymssp.2020.106795
Tsushima N., Su W. Flutter suppression for highly flexible wings using passive and active piezoelectric effects. Aerospace Science and Technology. 2017. Vol. 65. P. 78–89. DOI: 10.1016/j.ast.2017.02.013
Каменских А.О. Изменение собственных частот колебаний пьезоэлементами, встроенными в упругие тела. Известия РАН. МТТ. 2025. № 6. C. 261–276. DOI: 10.7868/S3034543X25060143
Almeida A., V. D.M., De Faria A.R., S.F.M. D.A. The effect of piezoelectrically induced stress stiffening on the aeroelastic stability of curved composite panels. Composite Structures. 2012. Vol. 94, no. 12. P. 3601–3611. DOI: 10.1016/j.compstruct.2012.06.008
Parton V.Z., Kudryavtsev B.A. Electromagnetoelasticity: Piezoelectrics and Electrically Conductive Solids [in Russian]. Moscow: Nauka, 1988. 470 p.
Zienkiewicz O.C., Taylor R.L. The finite element method. Vol. 1. 5th ed. Butterworth-Heinemann, 2000. 708 p.
Downloads
Published
Issue
Section
License
Copyright (c) 2026 Computational Continuum Mechanics

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.