首页 | 本学科首页   官方微博 | 高级检索  
     检索      

用敲击法识别位移模态和应变模态
引用本文:伊立言.用敲击法识别位移模态和应变模态[J].航空动力学报,1988,3(4):337-340,385.
作者姓名:伊立言
作者单位:南京航空学院
摘    要:本文提出了在振动模态试验中用电阻应变片直接识别位移模态和应变模态的理论和方法,提出应变导纳概念,建立了应变和振动位移的关系,推导出在振动系统中用应变量表示的传递函数公式。用本方法可以识别出系统的模态参数(包括应变模态、应力模态)。

收稿时间:5/1/1985 12:00:00 AM

STUDY ON DIRECT IDENTIFICATION OF DISPLACEMENT MODE AND STRAIN MODE BY IMPULSE EXCITATION
Yi Liyan.STUDY ON DIRECT IDENTIFICATION OF DISPLACEMENT MODE AND STRAIN MODE BY IMPULSE EXCITATION[J].Journal of Aerospace Power,1988,3(4):337-340,385.
Authors:Yi Liyan
Institution:Nanjing Aeronautical Institute
Abstract:The theory and method of direct identification of displacement and strain modes for vibration modal test with strain guages are described. The concept of strain mobility, strain displacement relationships and derivation of formulae of transfer functions in terms of strains are considered. The system modalparameters, including the strain mode and stress mode etc., can be identified by the present method. This is a new development for modal tests of impules excitation.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号