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

撞击平板的动力响应计算和实验研究
引用本文:杨治国,刘元镛,汤玄春,贾德新.撞击平板的动力响应计算和实验研究[J].航空学报,1992,13(6):258-265.
作者姓名:杨治国  刘元镛  汤玄春  贾德新
作者单位:西北工业大学504教研室 西安 710072
摘    要:本文采用16节点立体等参元,进行了冲击速度为10~20m/s时的平板动力响应数值分析。程序中考虑了结构的大变形,采用全拉格朗日描述法,时间离散使用了纽马克法。文中分别对LY12CZ和PMMA两种材料平板的动力响应计算结果和试验结果作了比较。提出用HopkinsonBar装置测定平板在硬撞击下撞击总耦合载荷及撞击点挠度随撞击时间的分布关系。同时文中提供了上述两种材料的动态力学性能参数,由这些参数可以认为PMMA为应变率敏感材料,在高速撞击下呈现“脆化”现象,而LY12CZ则为应变率不相关材料,在冲击载荷下呈现良好的塑性变形特性。

关 键 词:冲击载荷  霍普金森杆  应变速率  耦合载荷  
收稿时间:1990-04-20
修稿时间:1990-10-20

DYNAMIC RESPONSE ANALYSIS AND EXPERIMENTAL RESEARCH OF PLATE UNDER IMPACT LOAD
Yang Zhi-guo,Liu Yuan-yong,Tang Xuan-chun,Jia De-xin.DYNAMIC RESPONSE ANALYSIS AND EXPERIMENTAL RESEARCH OF PLATE UNDER IMPACT LOAD[J].Acta Aeronautica et Astronautica Sinica,1992,13(6):258-265.
Authors:Yang Zhi-guo  Liu Yuan-yong  Tang Xuan-chun  Jia De-xin
Institution:Faculty 504 of Northwestern pelytechnical University, Xi'an, 710072
Abstract:In this paper, the numerical analysis of dynamic response of the plate by cubic isoparametric elements of 16-nodes at 10~ 20 m / s impact rate is carried out. In the program the large deformation are considered by using Total Lagrange described method and time discreteness with Newmark method. A result of dynamic response calculation is compared with that of experiment for the plate of LY12CZ and PMMA respectively. A Hopkinson Bar device for measuring the coupling loads and deflection of impact points with impacting time is employed in this study. In the meantime, dynamic mechanical parameters of two materials mentioned above are provided, from which it shows that PMMA is a sensitive material to strain rate and appears brittleness' phenomenon, and LY12CZ is a material independent of strain rate and appears better plastic deformation behavior at impact loading.
Keywords:impact load  Hopkinson bar  strain rate  coupling load  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》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