Composite wing vibration coupling control
DOI:
https://doi.org/10.21638/spbu01.2023.214Abstract
The paper discusses the possibility to control coupled bending-twisting vibrations of composite wing by means of the monoclinic structures in the reinforcement of the plating. Decomposing the potential straining energy and kinetic energy of natural vibration modes into interacting and non-interacting parts, it became possible to introduce the two coefficients that integrally consider the effect of geometry and reinforcement structure upon the dynamic response parameters of the wing. The first of these coefficients describes the elastic coupling of the natural vibration modes, the second coefficient describes the inertial one. The paper describes the numerical studies showing how the orientation of considerably anisotropic CRP layers in the plating affects natural frequencies, loss factors, coefficients of elastic and inertial coupling for several lower tones of natural bending-twisting vibrations of the wing. Besides, for each vibration mode, partial values of the above mentioned dynamic response parameters were determined by means of the relationships for orthotropic structures where instead of “free” shearing modulus in the reinforcement plant, “pure” shearing modulus is used. Joint analysis of the obtained results has shown that each pair of bendingtwisting vibration modes has its orientation angle ranges of the reinforcing layers where the inertial coupling caused by asymmetry of the cross-section profile with respect to the main axes of inertia decreases, down to the complete extinction, due to the generation of the elastic coupling in the plating material. These ranges are characterized by the two main features: 1) the difference in the natural frequencies of the investigated pair of bendingtwisting vibration modes is the minimum and 2) natural frequencies of bending-twisting vibrations belong to a stretch restricted by corresponding partial natural frequencies of the investigated pair of vibration modes. This result is of practical importance because it enables approximate analysis of real composite wings with complex geometry in the existing commercial software packages.Keywords:
composite wing, coupled vibrations, elastic coupling, inertial connectivity, natural frequency, loss factors
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References
Литература
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2. Munk M. M. Patent US 2484308 А. Propeller containing diagonally disposed fibrous material. Publ. October, 11. 1949.
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5. Hayat K., de Lecea A. G. M., Moriones C. D., Ha S. K. Flutter performance of bend-twist coupled large-scale wind turbine blades. Journal of Sound and Vibration 370, 149-162 (2016).
6. Wang L., Kolios A., Nishino T., Delafin P.-L., Bird T. Structural optimisation of vertical-axis wind turbine composite blades based on finite element analysis and genetic algorithm. Composite Structures 153, 123-138 (2016).
7. Motley M. R., Barber R. B. Passive control of marine hydrokinetic turbine blades. Composite Structures 110, 133-139 (2014).
8. Li W., Zhou H., Liu H., Lin Y., Xu Q. Review on the blade design technologies of tidal current turbine. Renewable and Sustainable Energy Reviews 63, 414-422 (2016).
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10. Young Y. L. Dynamic hydroelastic scaling of self-adaptive composite marine rotors. Composite Structures 92, 97-106 (2010).
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Published
2023-05-10
How to Cite
Ryabov, V. M., & Yartsev, B. A. (2023). Composite wing vibration coupling control. Vestnik of Saint Petersburg University. Mathematics. Mechanics. Astronomy, 10(2), 344–356. https://doi.org/10.21638/spbu01.2023.214
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Articles of "Vestnik of Saint Petersburg University. Mathematics. Mechanics. Astronomy" are open access distributed under the terms of the License Agreement with Saint Petersburg State University, which permits to the authors unrestricted distribution and self-archiving free of charge.
