|Table of Contents|

The Finite Element Analysis for the Composite Rocket Launching Case(PDF)

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2000年05期
Page:
418-420
Research Field:
Publishing date:

Info

Title:
The Finite Element Analysis for the Composite Rocket Launching Case
Author(s):
SongYunxue ShiYongsheng WangXiaoming
School of Mechanics,NUST,Nanjing 210094
Keywords:
f inite element s composite materials st reng th rigidity
PACS:
-
DOI:
-
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.

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

Memo

Memo:
-
Last Update: 2013-03-25