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固体火箭发动机含裂纹药柱应力场有限元模拟的新方法

任海峰 高鸣

固体火箭技术Issue(1):50-54,5.
固体火箭技术Issue(1):50-54,5.DOI:10.7673/j.issn.1006-2793.2015.01.09

固体火箭发动机含裂纹药柱应力场有限元模拟的新方法

A new simulation method of 3D crack of solid rocket motor grain

任海峰 1高鸣1

作者信息

  • 1. 海军航空工程学院,烟台 264001
  • 折叠

摘要

Abstract

To study the variations in stress/strain field when the crack appears,a new technique to simulate 3D crack of solid rocket motor grain based on singular element and birth⁃death element was proposed. A part⁃through crack for solid rocket motor grain simulated by utilizing this method and stress distribution caused by crack were analyzed. Simulation results indicate that the method is correct,effective,and convenient for further research,especially suitable for comparative analysis on the stress distribution changes and the stress reliefs which are caused by crack or debond.

关键词

固体火箭发动机/药柱/奇异单元/生死单元/裂纹

Key words

solid rocket motor/grain/singular element/birth-death element/crack

分类

航空航天

引用本文复制引用

任海峰,高鸣..固体火箭发动机含裂纹药柱应力场有限元模拟的新方法[J].固体火箭技术,2015,(1):50-54,5.

基金项目

国防预研项目(51328050101)。 ()

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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