Synthesis of nonlinear frequency responses with experimentally extracted nonlinear modes

被引:37
|
作者
Peter, Simon [1 ]
Scheel, Maren [2 ]
Krack, Malte [2 ]
Leine, Remco I. [1 ]
机构
[1] Univ Stuttgart, Inst Nonlinear Mech, Pfaffenwaldring 9, D-70569 Stuttgart, Germany
[2] Univ Stuttgart, Inst Aircraft Prop Syst, Pfaffenwaldring 6, D-70569 Stuttgart, Germany
关键词
Nonlinear modes; Nonlinear system identification; Single nonlinear mode method; Nonlinear modal analysis; Nonlinear frequency response functions; MODAL-ANALYSIS; BACKBONE CURVES; IDENTIFICATION; SYSTEMS;
D O I
10.1016/j.ymssp.2017.09.014
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Determining frequency response curves is a common task in the vibration analysis of nonlinear systems. Measuring nonlinear frequency responses is often challenging and time consuming due to, e.g., coexisting stable or unstable vibration responses and structure exciter-interaction. The aim of the current paper is to develop a method for the synthesis of nonlinear frequency responses near an isolated resonance, based on data that can be easily and automatically obtained experimentally. The proposed purely experimental approach relies on (a) a standard linear modal analysis carried out at low vibration levels and (b) a phase-controlled tracking of the backbone curve of the considered forced resonance. From (b), the natural frequency and vibrational deflection shape are directly obtained as a function of the vibration level. Moreover, a damping measure can be extracted by power considerations or from the linear modal analysis. In accordance with the single nonlinear mode assumption, the near-resonant frequency response can then be synthesized using this data. The method is applied to a benchmark structure consisting of a cantilevered beam attached to a leaf spring undergoing large deflections. The results are compared with direct measurements of the frequency response. The proposed approach is fast, robust and provides a good estimate for the frequency response. It is also found that direct frequency response measurement is less robust due to bifurcations and using a sine sweep excitation with a conventional force controller leads to underestimation of maximum vibration response. (C) 2017 Elsevier Ltd. All rights reserved.
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页码:498 / 515
页数:18
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