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基于细观力学的复合固体推进剂模量预估方法
引用本文:李高春,邢耀国,王玉峰,庞爱民,郭翔,唐根.基于细观力学的复合固体推进剂模量预估方法[J].推进技术,2007,28(4):441-444.
作者姓名:李高春  邢耀国  王玉峰  庞爱民  郭翔  唐根
作者单位:1. 海军航空工程学院,飞行器工程系,山东,烟台,264001
2. 湖北红星化学研究所,湖北,襄樊,441003
摘    要:应用分子动力学方法得到了复合固体推进剂颗粒在基体内随机分布的填充模型。针对推进剂所含颗粒大小不同,采用细观力学有限元法和Mori-Tanaka分析法相结合的方法计算了推进剂的模量,计算所得模量与不同颗粒体积分数推进剂的单向拉伸试验结果比较吻合。此外,该方法可以获得推进剂细观结构应力,从而为推进剂的细观损伤分析奠定基础。

关 键 词:复合推进剂  有限元法  Mori-Tanaka法    杨氏模量
文章编号:1001-4055(2007)04-0441-04
收稿时间:2006-08-10
修稿时间:2007-01-08

A micromechanical method of the effective modulus estimation for the composite propellant
LI Gao-chun,XING Yao-guo,WANG Yu-feng,PANG Ai-min,GUO Xiang and TANG Gen.A micromechanical method of the effective modulus estimation for the composite propellant[J].Journal of Propulsion Technology,2007,28(4):441-444.
Authors:LI Gao-chun  XING Yao-guo  WANG Yu-feng  PANG Ai-min  GUO Xiang and TANG Gen
Institution:Department of Aircraft Engineering, Naval Aeronautical Engineering Academy, Yantai 264001, China; 2. Hubei Red Star Chemical Inst. , Xiangfan 441003, China
Abstract:The random distribution packing models of filler in the binder of composite solid propellant was generated based on the Molecular Dynamics(MD) method.By considering the different sizes of filler,the generated packing models were then analyzed by finite element method combined with the Mori-Tanaka method to evaluate the Young modulus of propellant.The numerical results agreed well with uniaxial tension experimental data on propellants with different volume fractions.Based on the new method,the stress field was determined,which provides the basis for micromechanical damage analysis.
Keywords:Composite propellant  Finite element method  Mori-Tanaka method  Young modulus
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