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固体推进剂药柱的近似不可压缩粘弹性随机有限元
引用本文:张书俊,任钧国,吴志桥.固体推进剂药柱的近似不可压缩粘弹性随机有限元[J].强度与环境,2006,33(2):33-38.
作者姓名:张书俊  任钧国  吴志桥
作者单位:国防科技大学航天与材料工程学院,长沙,410073
摘    要:采用Monte-Carlo粘弹性随机有限元法,分析了药柱的结构可靠度。针对固体火箭发动机药柱材料近似不可压缩的问题,基于Herrmann粘弹性有限元以提高计算的精度,考虑泊松比和松弛模量的随机性,采用拉丁超立方(LHS)技术计算了固体火箭发动机药柱结构的可靠度。算例表明该方法的有效性。

关 键 词:随机结构  可靠度  蒙特卡罗方法  拉丁超立方体抽样
文章编号:1006-3919(2006)02-0033-06
收稿时间:2005-12-01
修稿时间:2006-01-23

Structure dynamic reliability analysis of solid rocket motor viscoelasticity grains
ZHANG Shu-jun,REN Jun-guo,WU Zhi-qiao.Structure dynamic reliability analysis of solid rocket motor viscoelasticity grains[J].Structure & Environment Engineering,2006,33(2):33-38.
Authors:ZHANG Shu-jun  REN Jun-guo  WU Zhi-qiao
Institution:College of Aerospace and Material Engineering National Univ. of Defense Tech, Changsha 410073, China
Abstract:Structure reliability of grain was analyzed based on Monte Carlo viscoelastic stochastic finite element method. Nearly incompressible viscoelastic finite element method,is applied to increase the accuracy. Considering the randomness of Poisson ratio and relaxation modulus,structure reliability and its variational trend of the solid rocket motor grain under internal pressure was analyzed in contrast to general method. The results of evaluated examples demonstrate that this method is effective.
Keywords:stochastic structure  reliability  Monte Carlo method  latin hypercube sampling
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