A Method for Calculating the Dynamics of Rotating Flexible Structures, Part 2: Example Calculations

Author:

Segalman D. J.1,Dohrmann C. R.1,Slavin A. M.2

Affiliation:

1. Structural Dynamics and Controls Department, Sandia National Laboratories, Albuquerque, NM 87185

2. Solid and Structural Mechanics Department, Sandia National Laboratories, Albuquerque, NM 87185

Abstract

The problem of calculating the vibrations of rotating structures has challenged analysts since the observation that use of traditional modal coordinates in such problems leads to the prediction of instability involving infinite deformation when rotation rates exceed the first natural frequency. A method using a system of nonlinearly coupled deformation modes to analyze rotating general, linear (unjointed) structures that addresses the problem of erroneously predicting infinite deformations has been presented in a preceding paper (Segalman and Dohrmann, 1995). This technique is employed to address several types of problems ranging from simple beams to an inflated membrane structure. Some of the details of exploiting existing finite element codes to evaluate the relevant matrices are also developed.

Publisher

ASME International

Subject

General Engineering

Reference9 articles.

1. Blevins, R. D., 1979, Formulas for Natural Frequency and Mode Shape, Van Nostrand Reinhold Company, New York, pp. 108.

2. Cook, R. D., 1981, Concepts and Applications of Finite Element Analysis, John Wiley and Sons, New York, pp. 331–340.

3. Kane T. R. , RyanR. R., and BanerjeeA. K., 1987, “Dynamics of a Cantilever Beam Attached to a Moving Base,” AIAA J. Guidance, Control, and Dynamics, Vol. 10, pp. 139–151.

4. Segalman, D. J., and Dohrmann, C. R., 1990, “Dynamics of Rotating Flexible Structures by a Method of Quadratic Modes,” Sandia Report SAND90-2737, available through the National Technical Information Service, Springfield, VA.

5. Segalman, D. J., and Slavin, A. M., 1993, “Predicting the Vibrations of a Spinning Inflated Membrane,” Proceedings of 14th Biennial Conference On Mechanical Vibration And Noise, Albuquerque, Sept. 20–22.

Cited by 19 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

1. T-tail flutter simulations with regard to quadratic mode shape components;CEAS Aeronautical Journal;2021-06-18

2. Indirect reduced-order modelling: using nonlinear manifolds to conserve kinetic energy;Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences;2020-11

3. Accounting for Quasi-Static Coupling in Nonlinear Dynamic Reduced-Order Models;Journal of Computational and Nonlinear Dynamics;2020-04-29

4. A hybrid reduced-order modeling technique for nonlinear structural dynamic simulation;Aerospace Science and Technology;2019-01

5. Nonlinear Modal Substructuring of Panel and Stiffener Assemblies via Characteristic Constraint Modes;Dynamics of Coupled Structures, Volume 4;2017

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