PIAO Siyang, QI Feng, ZHANG Yahui. Model Updating for Large Structures Based on the Modal Synthesis Method[J]. Applied Mathematics and Mechanics, 2018, 39(9): 989-998. doi: 10.21656/1000-0887.390065
Citation: PIAO Siyang, QI Feng, ZHANG Yahui. Model Updating for Large Structures Based on the Modal Synthesis Method[J]. Applied Mathematics and Mechanics, 2018, 39(9): 989-998. doi: 10.21656/1000-0887.390065

Model Updating for Large Structures Based on the Modal Synthesis Method

doi: 10.21656/1000-0887.390065
Funds:  The National Natural Science Foundation of China(11672060)
  • Received Date: 2018-02-27
  • Publish Date: 2018-09-15
  • A synthetic technology for substructure test modeling was developed based on the finite element model updating theory and the modal synthesis method. During the substructure model updating, the fixed interface component modal synthesis method was adopted to reduce the substructure model, improve the computational efficiency and thereby promote the overall efficiency of the substructure test modeling. The steps of the design parameter method in model updating and the corresponding formulas based on the reduced model were given. With a launch vehicle model as the example, and by means of the secondary development of ANSYS, the present method gets verification of effectiveness.
  • loading
  • [1]
    王毅, 朱礼文, 王明宇, 等. 大型运载火箭动力学关键技术及其进展综述[J]. 导弹与航天运载技术, 2000(1): 29-37.(WANG Yi, ZHU Liwen, WANG Mingyu, et al. Summary of some key technologies on dynamics of large launch vehicle[J]. Missiles and Space Vehicles,2000(1): 29-37.(in Chinese))
    [2]
    邱吉宝, 王建民. 运载火箭模态试验仿真技术研究新进展[J]. 宇航学报, 2007,28(3): 515-521.(QIU Jibao, WANG Jianmin. The recent progresses on research into modal test simulation techniques for launch vehicles[J]. Journal of Astronautics,2007,28(3): 515-521.(in Chinese))
    [3]
    邱吉宝, 王建民. 航天器虚拟动态试验技术研究及展望[J]. 航天器环境工程, 2007,24(1): 1-14.(QIU Jibao, WANG Jianmin. A review on virtual dynamic test techniques for space vehicles[J]. Spacecraft Environmental Engineering,2007,24(1): 1-14.(in Chinese))
    [4]
    张正平, 邱吉宝, 王建民, 等. 航天器结构虚拟动态试验技术新进展[J]. 振动工程学报, 2008,21(3): 209-222.(ZHANG Zhengping, QIU Jibao, WANG Jianmin, et al. Progresses on virtual dynamic test techniques for space vehicles[J].Journal of Vibration Engineering,2008,21(3): 209-222.(in Chinese))
    [5]
    张德文. 未来大型复杂结构分析模型与试验状态的展望: 模型修正与模态综合技术的发展[J]. 强度与环境, 1988,15(6): 35-48, 53.(ZHANG Dewen. A review on analytical model and experimental state of large complex structures: development of model updating and modal synthesis techniques[J]. Structure & Environment Engineering,1988,15(6):35-48, 53.(in Chinese))
    [6]
    杜飞平, 谭永华, 陈建华. 基于子结构试验建模综合的火箭发动机结构动力分析[J]. 推进技术, 2015,36(10): 1547-1553.(DU Feiping, TAN Yonghua, CHEN Jianhua. Structural dynamic analysis of rocket engine based on synthetic technology for substructure test model[J]. Journal of Propulsion Technology,2015,36(10): 1547-1553.(in Chinese))
    [7]
    张亚辉, 林家浩. 结构动力学基础[M]. 大连: 大连理工大学出版社, 2007. (ZHANG Yahui, LIN Jiahao. Fundamentals of Structural Dynamics [M]. Dalian: Dalian University of Technology Press, 2007.(in Chinese))
    [8]
    HURTY W C. Vibrations of structural systems by component mode synthesis[J]. Journal of Engineering Mechanics Division,1960,86(4): 51-69.
    [9]
    CRAIG R R, BAMPTON M. Coupling of substructures for dynamic analysis[J]. AIAA Journal,1968,6(7): 1313-1319.
    [10]
    CASTANIER M P, TAN Y C, PIERRE C. Characteristic constraint modes for component mode synthesis[J]. AIAA Journal, 2001,39(6): 1182-1187.
    [11]
    SIMON D, COST T. Selection of characteristic constraint modes for component mode synthesis using a modification of effective interface mass[J]. AIAA Journal,2006,92(1): 248-263.
    [12]
    HOU S N. Review of modal synthesis techniques and a new approach[J]. Shock and Vibration Bulletin,1969,40(4): 25-30.
    [13]
    GOLDMAN R L. Vibration analysis by dynamic partitioning[J]. AIAA Journal,1969,7(6):1152-1154.
    [14]
    MACNEAL R H. A hybrid method of component mode synthesis[J]. Computers & Structures,1971,1(4): 581-601.
    [15]
    RUBIN S. Improved component-mode representation for structural dynamic analysis[J]. AIAA Journal,1975,13(8): 995-1006.
    [16]
    向树红, 邱吉宝, 王大钧. 模态分析与动态子结构方法新进展[J]. 力学进展, 2004,34(3): 289-303.(XIANG Shuhong, QIU Jibao, WANG Dajun. The resent progresses on modal analysis and dynamic sub-structure methods[J].Advances in Mechanics,2004,34(3): 289-303.(in Chinese))
    [17]
    BENFIELD W A, HRUDA R F. Vibration analysis of structures by component mode substitution[J].AIAA Journal,1971,9(7): 1255-1261.
    [18]
    楼梦麟. 结构动力分析的子结构方法[M]. 上海: 同济大学出版社, 1997.(LOU Menglin. Substructure Methods of Structural Vibration Analysis [M]. Shanghai: Tongji University Press, 1997.(in Chinese))
    [19]
    SUAREZ L E, SINGH M P. Improved fixed interface method for modal synthesis[J]. AIAA Journal,1992,30(12): 2952-2958.
    [20]
    QIU J B, YINGZ G, WILLIAMS F W. Exact modal synthesis techniques using residual constraint modes[J]. International Journal for Numerical Methods in Engineering,1997,40(13): 2475-2492.
    [21]
    张德文, 张欧骐. 关于固定界面法的一个附注: 精确固定界面法[J]. 振动与冲击, 1994,52(4): 15-22.(ZHANG Dewen, ZHANG Ouqi. Annotations on fixed-interface method: an accurate fixed-interface method[J]. Journal of Vibration and Shock,1994,52(4): 15-22.(in Chinese))
    [22]
    EWINS D J. Modal Testing: Theory and Practice [M]. Baldock: Research Studies Press, 2000.
    [23]
    ALLEMANG R J, BROWN D L, ROST R W. Experimental modal analysis and dynamic component synthesis, measurement techniques for experimental modal analysis: AFWAL TR 87-3069 volume 2[R]. Flight Dynamics Laboratory, 1987.
    [24]
    MOTTERSHEAD J E, LINK M, FRISWELL M I. The sensitivity method in finite element model updating: a tutorial[J]. Mechanical Systems and Signal Processing,2011,25(7): 2275-2296.
    [25]
    FRISWELL M I, MOTTERSHEAD J E. Finite Element Model Updating in Structural Dynamics [M]. Dordrecht: Kluwer Academic Publishers, 1995.
    [26]
    袁爱民. 基于灵敏度分析的有限元模型修正技术若干关键问题研究[D]. 博士学位论文. 南京: 东南大学, 2006.(YUAN Aimin. Studies on several key problems of finite element model updating based on the sensitivity analysis[D]. PhD Thesis. Nanjing: Southeast University, 2006.(in Chinese))
    [27]
    FRISWELL M I. Candidate reduced order models for structural parameter estimation[J]. Journal of Vibration and Acoustics,1990,112(1): 93-97.
    [28]
    NELSON R B. Simplified calculation of eigenvector derivatives[J]. AIAA Journal,1976,14(9): 1201-1205.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1332) PDF downloads(1542) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return