固体火箭发动机药柱三维温度场应力场有限元分析

推进技术 ›› 1997, Vol. 18 ›› Issue (2): 21-26.

固体火箭发动机药柱三维温度场应力场有限元分析

朱智春,蔡峨

北京航空航天大学宇航学院!北京;100083;北京航空航天大学宇航学院!北京;100083

发布日期:2021-08-15
基金资助:
航空科学基金

A FINITE ELEMENT ANALYSIS OF THREE DIMENSIONAL TEMPERATURE AND STRESS FIELDS FOR SOLID ROCKET MOTOR GRAIN

School of Astronautics, BeiJing Univ. of Aeronautics and Astronautics, Beijing, 100083;School of Astronautics, BeiJing Univ. of Aeronautics and Astronautics, Beijing, 100083

Published:2021-08-15

摘要/Abstract

摘要： 采用有限元法计算固体火箭发动机药柱在固化冷却时的三维瞬态温度场。基于粘弹性积分型本构关系，计算热应力场。计算程序可用于工程实际。

关键词: 固体推进剂火箭发动机;推进剂药柱;温度分布;应力分布;有限元法

Abstract: The transient temperature distribution in a solid rocket motor grain during its curingprocess is calculated with three dimensional finite element method. Based on the viscoelastic integralconstitutive relation, a thermal stress field in the grain is calculated, and the calculating program maybe used in engineering practice.

Key words: Solid propellant rocket engine;Propellant grain;Temperature distribution;Stress distribution;Finite element method

朱智春,蔡峨. 固体火箭发动机药柱三维温度场应力场有限元分析[J]. 推进技术, 1997, 18(2): 21-26.

固体火箭发动机药柱三维温度场应力场有限元分析

A FINITE ELEMENT ANALYSIS OF THREE DIMENSIONAL TEMPERATURE AND STRESS FIELDS FOR SOLID ROCKET MOTOR GRAIN

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