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

导弹垂直弹射过程中制动锥的动力学特性研究
引用本文:毕世华,王汉平,梁征.导弹垂直弹射过程中制动锥的动力学特性研究[J].北京理工大学学报,2004,24(9):762-765.
作者姓名:毕世华  王汉平  梁征
作者单位:北京理工大学,机电工程学院,北京,100081;北京理工大学,机电工程学院,北京,100081;北京理工大学,机电工程学院,北京,100081
基金项目:高等学校博士学科点专项科研项目
摘    要:研究导弹垂直弹射过程中制动锥的动力学行为.基于塑性铰理论,利用功能原理和能量守恒定律进行理论分析;采用非线性有限元软件ABAQUS进行仿真计算;采用准静态方式完成了压力机上的试验.用3种方法所得结果基本一致.有限元计算和试验结果给出了接触力和制动锥压缩量之间的经验公式,具体结果和结论可用于制动锥的工程设计和武器系统的发射动力学分析.

关 键 词:导弹垂直弹射装置  制动锥  有限元方法  渐进屈曲  结构冲击
文章编号:1001-0645(2004)09-0762-04
收稿时间:2003/11/22 0:00:00
修稿时间:2003年11月22日

A Study on the Dynamical Characteristics of the Braking Cylindrical Shells During the Vertical Ejection of Missiles
BI Shi-hu,WANG Han-ping and LIANG Zheng.A Study on the Dynamical Characteristics of the Braking Cylindrical Shells During the Vertical Ejection of Missiles[J].Journal of Beijing Institute of Technology(Natural Science Edition),2004,24(9):762-765.
Authors:BI Shi-hu  WANG Han-ping and LIANG Zheng
Institution:School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China;School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China;School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China
Abstract:The dynamical behavior of the braking cylindrical shells during the vertical ejection of missiles has been studied. On the basis of plastic joint theory, theoretical analysis was carried out using work-energy principle and energy conservation theorem. Computations were completed using the nonlinear FEM software ABAQUS. Experiments were accomplished on the press in a quasi-static state. Results from the above three methods were found essentially identical. An empirical formula relating the contact force to the compression deformation of the braking cylindrical shells is given using the results of computation and experiment. The empirical formula can be used in the engineering design of the braking cylindrical shells and in the launching dynamics analysis of the weapon system.
Keywords:vertical ejection launcher for missiles  braking cylindrical shell  FEM  asymptotic buckling  structural impact
本文献已被 CNKI 维普 万方数据 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