期刊文献+

均匀流场拉条模型颤振导数识别试验研究 被引量:3

Testing study of determination of flutter derivatives by taut strip model in smooth flow
下载PDF
导出
摘要 拉条模型作为介于全桥气弹模型和节段模型之间的一种气弹模型,在以往的研究中,常用来比较分析节段模型和全桥气弹模型试验结果的差异而使用,而没有利用该模型进行主梁断面颤振导数识别的研究报道。本文则引入模态参数识别方法进行拉条模型颤振导数识别,并设计了一个平板断面的拉条模型,在均匀流场下进行了颤振导数识别试验研究,与理想平板颤振导数理论解进行了比较,试验结果与理论解的吻合说明了拉条模型颤振导数识别方法的可靠性。 Taut strip model is an aeroelastic model, which can be regarded as in-between model between sectional model and full aeroelastic bridge model. In old practice, the model was used to compare the difference of the results between sectional models and full aeroelastic models. Determination of flutter derivatives by taut strip model has rarely been studied. In this paper, modal parameter identification technique is introduced into identification of flutter derivatives by taut strip model. A thin-plat taut strip model is designed, and it is used in smooth flow to determine flutter derivatives. In the end, comparison with theoretical flutter derivatives of thin plate section is undertaken to validate the reliability of the theory.
出处 《空气动力学学报》 EI CSCD 北大核心 2006年第2期147-151,168,共6页 Acta Aerodynamica Sinica
基金 国家自然科学基金重大资助项目(50478109) 高等学校博士学科点专项科研基金资助项目(2004027026)
关键词 拉条模型 颤振导数识别 均匀流场 taut strip model flutter derivatives smooth flow
  • 相关文献

参考文献15

  • 1SCANLAN R H,TOMKO J J.Airfoil and Bridge Deck Flutter Derivatives[ J ].J.Eng.Mech.,ASCE,1971,97 (6):1717-1737.
  • 2KUMARASENA T,SCANLAN R H,BOSCH H R.Wind response prediction of flexible bridges[ C ].Proceedings sixth US National Conference on wind engineering,March,1989.
  • 3SHINOZUKA M,YUN C B,IMAI H.Identification of linear structural dynamic systems[ J ].Journal of the Engineering Mechanics Division,1982,108(6):1371-1890.
  • 4YAMADA H,ICHIKAWA H.Estimation of aerodynamics parameters by extended kalman filter algorithm[ J ].J.Wind.Eng.1989,41.
  • 5SARKAR P P.Identification of aeroelastic parameters of flexible bridge[J].J.Eng.Mech.,ASCE,1994,120(8):1718-1741.
  • 6GUM,ZHANGRX,XIANGHF.Parametricstudyonflutter derivatives of bridge decks[ J ].Engineering Structures,2001,23:1607-1613.
  • 7张令弥.柔性桥梁非定常气动导数识别研究[R].土木工程防灾国家重点实验室开放课题研究,2001.
  • 8QIN X R,GU M.Determination of flutter derivatives by covariance-driven stochastic subspace identification technique[J].Wind and Structure,2004,7(3):173-186.
  • 9CHOWDHURY A G,SARKAR P P.Identification of eighteen flutter derivatives of an airfoil and a bridge deck[ J ].Wind and Structure,2004,7 (3):187-202.
  • 10ZASSO A,NEGRI C S.Flutter derivatives identification through full bridge aeroelastic model transfer function analysis[J].J.Wind Eng.&Ind.Aerodynamics,1996,60:17-33.

同被引文献15

  • 1樊可清,倪一清,高赞明.改进随机子空间系统辨识方法及其在桥梁状态监测中的应用[J].中国公路学报,2004,17(4):70-73. 被引量:17
  • 2王卫华,李明水,陈忻.强迫振动法提取桥梁气动导数研究[J].实验流体力学,2005,19(1):47-51. 被引量:1
  • 3常军,张启伟,孙利民.随机子空间方法在桥塔模态参数识别中的应用[J].地震工程与工程振动,2006,26(5):183-187. 被引量:11
  • 4许福友.桥梁结构颤振导数识别与颤振分析[D].上海:同济大学桥梁工程系,2006.
  • 5陈艾荣.苏通大桥全桥气弹模型风洞试验研究[R].上海:同济大学,2004.
  • 6Diana G, Cheli F, Zasso A. Suspension bridge parameter identification in full scale test [J]. J. Wind Eng. Ind. Aerodyn., 1992, 41-44:165-176.
  • 7Zasso A, Negri C S . Flutter derivatives identification through full bridge aeroelasfic model transfer function analysis [J]. J. Wind Eng. Ind. Aerodyn., 1996, 60:17-33.
  • 8Qin X R, Gu M. Determination of flutter derivatives by covariance-driven stochastic subspace identification technique [J].Wind and Structures, 2004, 7(3): 173-186.
  • 9Qin X R,Gu M.Determination of flutter derivatives by covariance-driven stochastic subspace identification technique[J].Wind and Structures,2004,7(3):173-186
  • 10Peeters B,Roeck G.Comparison of system identification methods using operational data of a bridge test[C]//Proceedings of ISMA 23,noise and vibration engineering.1998:923-930

引证文献3

二级引证文献12

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