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

引信典型支承板受冲击载荷作用时的非线性动力分析
引用本文:高世桥,臧岩.引信典型支承板受冲击载荷作用时的非线性动力分析[J].北京理工大学学报,1996,16(4):395-400.
作者姓名:高世桥  臧岩
作者单位:北京理工大学机电工程系
摘    要:在建立引信典型支承板非线性动力变弯曲模型基础上,采用的摄动法处理了非线性的问题,采用中心差分法开辟了一般模态分析的途径;采用模态叠加法解决了受迫振动的响应分析问题。文中对飞航导弹引信支承板的非线性动力响应进行了分析和计算。

关 键 词:非线性  动力响应  支承板经上信  冲击载荷

Nonlinear Dynamic Analysis of a Typical Fuze Supporting Plate Considering Shock Loading
Gao Shiqho,Zang Yan,Tan Huimin.Nonlinear Dynamic Analysis of a Typical Fuze Supporting Plate Considering Shock Loading[J].Journal of Beijing Institute of Technology(Natural Science Edition),1996,16(4):395-400.
Authors:Gao Shiqho  Zang Yan  Tan Huimin
Abstract:On the basis of nonlinear dynamic bending model of a typica fuze supporting plate, the nonlinear problem is disposed using the perturbation perturbation method and the way of general medal analysis is opened up using the central difference metjod.The problem of response analysis for the forced vibrations is settled using the modal superposition method. As an example,the nonlinear dynamic response of the supporting plate of a missile fuze has been analysed and calculated.
Keywords:nonlinearity  dynamic response  circular thin plate  shock
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《北京理工大学学报》浏览原始摘要信息
点击此处可从《北京理工大学学报》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