期刊文献+

屈曲薄膜振动分析 被引量:5

VIBRATIONS ANALYSIS OF BUCKLING MEMBRANE
下载PDF
导出
摘要 非线性大变形屈曲分析是处理薄膜褶皱问题的一种有效方法,该文对这种方法的两个关键问题进行了探讨,包括初始缺陷的施加及后屈曲平衡路径的跟踪。基于这种方法分析了剪切薄膜的褶皱,并在褶皱构形的基础上,进行了考虑大变形效应的模态分析。分析结果表明:具有褶皱薄膜振动的模态及固有频率与不具有褶皱的薄膜相比明显的不同,褶皱薄膜的固有频率明显的减小了,其节线的位置为张拉线的位置,随着模态的增加其节线的数目减少。该文所建立的分析过程,不但能够进行薄膜褶皱的分析,同时也能分析褶皱形成后薄膜的动态特性。 Nonlinear large deformation buckling analysis is an effective method dealing with membrane wrinkle problems. Two key issues of this method, the introduction of original flaw and the follow of post-buckling balance path, are discussed in this paper. According to this method, wrinkles of shear membrane are analyzed. Based on wrinkle configuration, modal analysis is performed with the consideration of the large deformation. The result indicates that the modal and natural frequency of the membrane with wrinkles are obvious different from the membrane without wrinkles. The natural frequency is decrease sharply; the position of pitch lines are that of tensile lines, and the number of pitch lines is decrease as mode increased. The analytical process established in the paper can be used for membrane wrinkles prediction and dynamic characteristics analysis with wrinkles.
出处 《工程力学》 EI CSCD 北大核心 2008年第11期33-36,85,共5页 Engineering Mechanics
关键词 薄膜 褶皱 后屈曲 动态分析 数值方法 membrane Wrinkling post-buckling dynamic analysis numerical method
  • 相关文献

参考文献12

  • 1Freeland R E, Bilyeu G D, Veal G R. Large inflatable deployable antenna flight experiment results [J]. Acta Astronautica, 1997, 41(4-10): 267-277.
  • 2Freeland R E, Bilyeu G D, Veal G R. Development of flight hardware for a large, inflatable-deployable antenna experiment [J]. Acta Astronautica, 1996, 38(4-8): 251 - 260.
  • 3Murphy D, Murphey T, Gierow P. Scalable solar-sail subsystem design concept [J]. AIAA Journal of Spacecraft and Rockets, 2003, 40(4): 539-547.
  • 4Grossman G, Williams G. Inflatable concentrators for solar propulsion and dynamic space power [J]. Journal of Solar Energy Engineering, 1990, 112(4): 229-236.
  • 5Akahoshi Y, Nakamura R, Tanaka M. Development of bumper shield using low density materials [J]. International Journal of Impact Engineering, 2001, 26(1-10): 13- 19.
  • 6Thomas W, Murphey, David M, Murphy. A method to quantify the thrust degradation effects of structural wrinkles in solar sails [C]. 43rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference Online Proceedings. Denver, Colorado, 2002.
  • 7Hossain N M A, Jenkins C H. Transverse vibration analysis for partly wrinkled membranes [J]. Journal of Spacecraft and Rockets, 2006, 43(3): 626-637.
  • 8杜星文,王长国,万志敏.空间薄膜结构的褶皱研究进展[J].力学进展,2006,36(2):187-199. 被引量:15
  • 9谭锋,杨庆山,张建.薄膜结构褶皱分析的有限元法[J].工程力学,2006,23(A01):62-68. 被引量:12
  • 10Roddeman D G, Drukker J, Oomens C W, Janssen J D. The Wrinkling of thin membranes: Part Ⅰ-Theory [J]. Journal of Applied Mechanics, 1987, 54: 884-887.

二级参考文献68

  • 1李作为,杨庆山,刘瑞霞.薄膜结构褶皱研究述评[J].中国安全科学学报,2004,14(7):16-20. 被引量:13
  • 2谭锋,杨庆山,李作为.薄膜结构分析中的褶皱判别准则及其分析方法[J].北京交通大学学报,2006,30(1):35-39. 被引量:17
  • 3Freeland R E,Bilyeu G D,Veal G R.Large inflatable deployable antenna flight experiment results.IAF-97-1301,1997.
  • 4Pellegrino S,Green C,Guest S D,Watt A.SAR advanced deployable structure.Technique Report CUED/DSTRUCT/TR191,University of Cambridge,Department of Engineering,Cambridge,UK,2000.
  • 5Leipold M.Solar sail technology ground and in-orbit deployment testing.In:Royal Astronomical Society Discussion Meeting,2002-05-10.2002.
  • 6Stockman H S.The next generation space telescope.Report for EESA,1997.
  • 7Pellegrino S.Collapsible rib-tensioned surface (crts) technology development.European Space Agency Contractor finial Report CUED/D-STRUCT/TR195,2001-04-02.2001.
  • 8Tibert A G,Pellegrino S.Furlable reflector concept for small satellites.AIAA-2001-1261,2001.
  • 9Wagner H.Flat sheet metal girders with very thin metal webs.Parts ⅠⅡⅢ,NACA Tech Memoranda,Nos 1929.20,200~314.
  • 10Reissner E.On tension field theory.In:Proceedings of the 5th International Congress of Applied Mechanics,Cambridge USA,1938.88~92.

共引文献24

同被引文献36

  • 1谭惠丰,李云良.薄膜后屈曲振动行为分析[J].哈尔滨工业大学学报,2011,43(S1):61-65. 被引量:3
  • 2Tan Huifeng, Li Yunliang. Analysis of post-bucklingdynamic behavior of membrane [J]. Journal of HarbinInstitute of Technology, 2011, Sup43(l): 61-65.
  • 3Kukathasan S, Pellegrino S. Nonlinear vibration ofwrinkled membranes [C]. Norfolk, Virginia. Proceedingof the 44th AIAA SDM Conference. 7-10 April 2003,AIAA 2003-1747.
  • 4Hossain N M A. Wrinkles and gravity effects ontransverse vibration of membranes [C]. Austin, Texas.Proceeding of the 46th AIAA SDM Conference. 18-21April 2005,AIAA 2005-1978,.
  • 5Ala Tabiei, Romil Tanov. A nonlinear higher order sheardeformation shell element for dynamic explicit analysis:Part, formulation and finite element equations [J]. FiniteElements in Analysis and Design, 2000,36(1): 17-37.
  • 6泰德.彼莱奇科,廖荣锦,布莱恩.莫兰.连续体和结构的非线性有限元[M].庄茁,译.北京:清华大学出版社,2002: 126-128.
  • 7Ted Belytschko, Wing Kam Liu, Brian Moran. Nonlinearfinite elements for continual and structutrs [M].Transtated by Zhuangzhuo. Beijing: Tsinghua UniversityPress, 2002: 126-128.
  • 81991-2005, LS-DYNA theoretical manual [S]. LivermoreCalifornia. Livermore Software Technology Corportation.2005.
  • 9Zhao Haiou. Guide to dynamic analysis of LS-DYNA[M]. Beijing: Weapon Industry Press, 2003: 16-20.
  • 10Hang Yuying. Structure vibration analysis [M]. Wuhan:Huazhong institute of Technology Press, 1988: 148 - 155.

引证文献5

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部