TY - JOUR
T1 - Rate-dependent bifurcation dodging in a thermoacoustic system driven by colored noise
AU - Zhang, Xiaoyu
AU - Xu, Yong
AU - Liu, Qi
AU - Kurths, Jürgen
AU - Grebogi, Celso
N1 - Acknowledgments
This paper was supported by the National Natural Science Foundation of China under Grant No.11772255 and No.12072264, the National Key Research and Development Program of China (No. 2018AAA0102201), the Fundamental Research Funds for the Central Universities, the Research Funds for Interdisciplinary Subject of Northwestern Polytechnical University, the Shaanxi Project for Distinguished Young Scholars, and Shaanxi Provincial Key R&D Program 2020KW-013 and 2019TD-010.
PY - 2021/5/31
Y1 - 2021/5/31
N2 - Tipping in multistable systems occurs usually by varying the input slightly, resulting in the output switching to an often unsatisfactory state. This phenomenon is manifested in thermoacoustic systems. This thermoacoustic instability may lead to the disintegration of rocket engines, gas turbines and aeroengines, so it is necessary to design control measures for its suppression. It was speculated that such unwanted instability states may be dodged by changing quickly enough the bifurcation parameters. Thus, in this work, based on a fundamental mathematical model of thermoacoustic systems driven by colored noise, the corresponding Fokker-Planck-Kolmogorov equation of the amplitude is derived by using a stochastic averaging method. A transient dynamical behavior is identified through a probability density analysis. We find that the rate of change of parameters and the correlation time of the noise are helpful to dodge thermoacoustic instability, while a relatively large noise intensity is a disadvantageous factor. In addition, power-law relationships between the maximum amplitude and the noise parameters are explored, and the probability of successfully dodging a thermoacoustic instability is calculated. These results serve as a guide to the design of engines and to propose an effective control strategy, which is of great significance to aerospace-related fields.
AB - Tipping in multistable systems occurs usually by varying the input slightly, resulting in the output switching to an often unsatisfactory state. This phenomenon is manifested in thermoacoustic systems. This thermoacoustic instability may lead to the disintegration of rocket engines, gas turbines and aeroengines, so it is necessary to design control measures for its suppression. It was speculated that such unwanted instability states may be dodged by changing quickly enough the bifurcation parameters. Thus, in this work, based on a fundamental mathematical model of thermoacoustic systems driven by colored noise, the corresponding Fokker-Planck-Kolmogorov equation of the amplitude is derived by using a stochastic averaging method. A transient dynamical behavior is identified through a probability density analysis. We find that the rate of change of parameters and the correlation time of the noise are helpful to dodge thermoacoustic instability, while a relatively large noise intensity is a disadvantageous factor. In addition, power-law relationships between the maximum amplitude and the noise parameters are explored, and the probability of successfully dodging a thermoacoustic instability is calculated. These results serve as a guide to the design of engines and to propose an effective control strategy, which is of great significance to aerospace-related fields.
KW - thermoacoustic system
KW - colored noise
KW - rate-dependent tipping
KW - transient
U2 - 10.1007/s11071-021-06368-5
DO - 10.1007/s11071-021-06368-5
M3 - Article
VL - 104
SP - 2733
EP - 2743
JO - Nonlinear Dynamics
JF - Nonlinear Dynamics
SN - 0924-090X
ER -