Self-Excited Vibrations and Damping in Circulatory Systems

Author:

Hagedorn Peter1,Eckstein Manuel2,Heffel Eduard2,Wagner Andreas2

Affiliation:

1. Professor Fellow ASME Dynamics and Vibrations Group, Numerical Methods in Mechanical Engineering, Technische Universität Darmstadt, Dolivostr. 15, Darmstadt 64293, Germany e-mail:

2. Dynamics and Vibrations Group, Numerical Methods in Mechanical Engineering, Technische Universität Darmstadt, Dolivostr. 15, Darmstadt 64293, Germany e-mail:

Abstract

Self-excited vibrations in mechanical engineering systems are in general unwanted and sometimes dangerous. There are many systems exhibiting self-excited vibrations which up to this day cannot be completely avoided, such as brake squeal, the galloping vibrations of overhead transmission lines, the ground resonance in helicopters and others. These systems have in common that in the linearized equations of motion the self-excitation terms are given by nonconservative, circulatory forces. It has been well known for some time, that such systems are very sensitive to damping. Recently, several new theorems concerning the effect of damping on the stability and on the self-excited vibrations were proved by some of the authors. The present paper discusses these new mathematical results for practical mechanical engineering systems. It turns out that the structure of the damping matrix is of utmost importance, and the common assumption, namely, representing the damping matrix as a linear combination of the mass and the stiffness matrices, may give completely misleading results for the problem of instability and the onset of self-excited vibrations. The authors give some indications on improving the description of the damping matrix in the linearized problems, in order to enhance the modeling of the self-excited vibrations. The improved models should lead to a better understanding of these unwanted phenomena and possibly also to designs oriented toward their avoidance.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference38 articles.

1. Rafanello, S., 1999, “Modeling the Coupled Rotor/Fuselage Response of the H-3 Sea King Utilizing the NPS Full Nonlinear Response,” M.S. thesis, Naval Postgraduate School, Monterey, CA.

2. Wang, W., 2007, “Semi-Active Adaptive Control of Helicopter Ground Resonance,” Ph.D. thesis, Nanjing University of Aeronautics and Astronautics, Nanjing, China.

3. Mokrane, A., 2011, “Helicopter Ground Resonance Prediction Using an Integrated Nonlinear Model,” Ph.D. thesis, University of Bristol, Bristol, UK.

4. Sanches, L., 2011, “Helicopter Ground Resonance: Dynamical Modeling, Parametric Robustness Analysis and Experimental Validation,” Ph.D. thesis, Université de Toulouse, Toulouse, France.

5. Eckert, B., 2007, “Analytical and Numerical Ground Resonance Analysis of a Conventionally Articulated Main Rotor Helicopter,” M.S. thesis, Department of Mechanical Engineering, Stellenbosch University, Stellenbosch, South Africa.

Cited by 21 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3