[1]宋云雪,史永胜,王晓鸣.复合材料火箭发射管有限元分析[J].南京理工大学学报(自然科学版),2000,(05):418-420.
 SongYunxue ShiYongsheng WangXiaoming.The Finite Element Analysis for the Composite Rocket Launching Case[J].Journal of Nanjing University of Science and Technology,2000,(05):418-420.
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复合材料火箭发射管有限元分析()
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
期数:
2000年05期
页码:
418-420
栏目:
出版日期:
2000-10-30

文章信息/Info

Title:
The Finite Element Analysis for the Composite Rocket Launching Case
作者:
宋云雪史永胜王晓鸣
南京理工大学机械学院, 南京210094
Author(s):
SongYunxue ShiYongsheng WangXiaoming
School of Mechanics,NUST,Nanjing 210094
关键词:
有限元 复合材料 强度 刚度
Keywords:
f inite element s composite materials st reng th rigidity
摘要:
该文基于复合材料单元运用有限元方法 ,构建了复合材料火箭发射管的有限元分析模型 ,全面分析了复合材料火箭发射管的结构特征 ,研究了发射管的火箭效应 ,分析了它的应力分布、刚度及强度 ,为复合材料在火箭发射管中的应用提供了理论基础
Abstract:
Based on composite element, the paper builds finite element s analysis model of the composite rocket launching case by using f inite elements method, completely analyses st ructure character of the composite rocket launching case and studies the rocket inherent ef fect on the launching case, analyses dist ribut ion of stress, rigidity and st reng th, it provides the theoretical basis for the composite use in rocket launching case.

参考文献/References:

1 朱壮瑞, 孙凌玉.基于动力学模型的轻型客车白车身工况响应分析. 东南大学学报, 1999
( 6) : 95~ 992 王永岩. 动态子结构方法理论及应用. 北京: 科学出版社, 1999

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备注/Memo

备注/Memo:
宋云雪 女 32 岁 硕士生
更新日期/Last Update: 2013-03-25