Abstract
In this study, time-delayed feedback control is investigated for an elastically mounted rectangular prism undergoing subcritical galloping in the transverse direction, when subjected to wind excitation. The mathematical model of the galloping system under consideration is established by using the quasi-steady aerodynamic theory. The control performance in terms of the galloping onset speed of the time-delayed displacement, velocity and acceleration feedback is investigated via linear stability analysis, respectively. Subsequently, the method of multiple scales is implemented for nonlinear analysis in order to derive the analytical expression of the vibration amplitude of the galloping system and determine the criticality curve that is the boundary of the subcritical and supercritical bifurcation regions. The results show that the hybrid objective of increasing the galloping onset speed, changing the Hopf bifurcation behavior from subcritical to supercritical and reducing the amplitude of limit-cycle oscillations can be achieved by means of delayed acceleration feedback. This study provides an analytical tool and procedure for time-delayed feedback control design of such a kind of flow–structure interaction system.
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Acknowledgements
This work was supported by the National Science Foundation of Jiangsu Province (Grant No. BK20190664) and the National Natural Science Foundation of China (Grant No. 11902146). The authors wish to thank Associate Prof. Zhang Li of Nanjing University of Aeronautics and Astronautics for her support on the numerical simulation of the neutral-type time-delay system.
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Liu, H., Gao, X. Analytical study of time-delayed feedback control of rectangular prisms undergoing subcritical galloping. Nonlinear Dyn 103, 103–114 (2021). https://doi.org/10.1007/s11071-020-06103-6
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DOI: https://doi.org/10.1007/s11071-020-06103-6