Moment Lyapunov exponent and stochastic stability of binary airfoil driven by non-Gaussian colored noise

被引:28
作者
Hu, D. L. [1 ]
Huang, Y. [1 ]
Liu, X. B. [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Coll Aerosp Engn, Nanjing 210016, Jiangsu, Peoples R China
基金
中国国家自然科学基金; 高等学校博士学科点专项科研基金;
关键词
Moment Lyapunov exponent; Stochastic stability; Perturbation method; Non-Gaussian colored noise; Monte Carlo simulation; COUPLED OSCILLATORS DRIVEN; FLUTTER; ENHANCEMENT; RESONANCE; SYSTEM;
D O I
10.1007/s11071-012-0577-x
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, the moment Lyapunov exponent and stochastic stability of binary airfoil subjected to non-Gaussian colored noise are investigated. The noise is simplified to an Ornstein-Uhlenbeck process by applying a path-integral approach. Via the singular perturbation method, the second-order expansions of the moment Lyapunov exponent are obtained, which agree with the results obtained using the Monte Carlo simulation well. Finally, the effects of the noise and system parameters on the stochastic stability of the binary airfoil system are discussed.
引用
收藏
页码:1847 / 1859
页数:13
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