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考虑人工脱粘层接触效应的药柱粘弹性分析

岳健 邓斌 申志彬 李道奎

固体火箭技术2013,Vol.36Issue(3):338-341,352,5.
固体火箭技术2013,Vol.36Issue(3):338-341,352,5.DOI:10.7673/j.issn.1006-2793.2013.03.010

考虑人工脱粘层接触效应的药柱粘弹性分析

Viscoelastic analysis of solid motor grain considering contact effect between stress release boots

岳健 1邓斌 1申志彬 1李道奎1

作者信息

  • 1. 国防科技大学航天科学与工程学院,长沙410073
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摘要

Abstract

Considering contact effect between stress release boots,finite element software MSC.Patran/Marc was used as a tool to make a viscoelastic analysis of two stage solid motor under axial overload condition.Von Mises stress/strain of motor grain under eight cases was compared to analyze the performance of contact effect in dynamic and static mode.A simple method of judging the necessity of considering the contact effect was obtained.The results show that the numerical values of Von Mises stress/strain considering contact effect between stress release boots were higher than that without considering contact effect; the numerical values of Von Mises stress/strain in dynamic mode were higher than that in static mode; the results in dynamic mode were more accurate for the simulation calculation of the contact effect.Some conclusions obtained and the analysis methods provide reference for the design and development of solid motors.

关键词

接触效应/固体火箭发动机/有限元法/人工脱粘层/粘弹性

Key words

contact effect/ solid rocket motor/ finite element method/ stress release boot / viscoelasticity

分类

航空航天

引用本文复制引用

岳健,邓斌,申志彬,李道奎..考虑人工脱粘层接触效应的药柱粘弹性分析[J].固体火箭技术,2013,36(3):338-341,352,5.

基金项目

国家自然科学基金(11272348). (11272348)

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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