Steady-state regimes prediction of a multi-degree-of-freedom unstable dynamical system coupled to a set of nonlinear energy sinks

被引:19
作者
Bergeot, Baptiste [1 ]
Bellizzi, Sergio [2 ]
机构
[1] Univ Tours, Univ Orleans, INSA CVL, LaMe EA 7494, 3 Rue Chocolaterie,CS 23410, F-41034 Blois, France
[2] Aix Marseille Univ, Cent Marseille, CNRS, LMA UMR 7031, Marseille, France
关键词
Multi-degree-of-freedom unstable system; Set of nonlinear energy sinks; Passive mitigation; Relaxation oscillations; Mitigation limit; Asymptotic analysis; MECHANICAL OSCILLATORS; ASYMPTOTIC ANALYSIS; SUPPRESSION; INSTABILITY; VIBRATION; PARALLEL; MITIGATION;
D O I
10.1016/j.ymssp.2019.05.045
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A general method to predict the steady-state regimes of a multi-degree-of-freedom unstable vibrating system (the primary system) coupled to several nonlinear energy sinks (NESs) is proposed. The method has three main steps. The first step consists in the diagonalization of the primary underline linear system using the so-called biorthogonal transformation. Within the assumption of a primary system with only one unstable mode the dynamics of the diagonalized system is reduced ignoring the stable modes and keeping only the unstable mode. The complexification method is applied in the second step with the aim of obtaining the slow-flow of the reduced system. Then, the third step is an asymptotic analysis of the slow-flow based geometric singular perturbation theory. The analysis shows that the critical manifold of the system can be reduced to a one dimensional parametric curve evolving in a multidimensional space. The shape and the stability properties of the critical manifold and the stability properties of the fixed points of the slow-flow provide an analytical tool to predict the nature of the possible steady-state regimes of the system. Finally, two examples are considered to evaluate the effectiveness and advancement of the proposed method. The method is first applied to the prediction of the mitigation limit of a breaking system subject to friction-induced vibrations coupled to two NESs, and next an airfoil model undergoing an aeroelastic instability coupled to a NESs setup (from one to four) is discussed. Theoretical results are compared, for validation purposes, to direct numerical integration of the system. The comparisons show good agreement. (C) 2019 Elsevier Ltd. All rights reserved.
引用
收藏
页码:728 / 750
页数:23
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