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改进的Mori-Tanaka法在复合推进剂非线性界面脱粘中的应用
引用本文:刘承武,阳建红,陈飞.改进的Mori-Tanaka法在复合推进剂非线性界面脱粘中的应用[J].固体火箭技术,2011,34(1):67-70.
作者姓名:刘承武  阳建红  陈飞
作者单位:第二炮兵工程学院,西安,710025
基金项目:国防973项目(61338)
摘    要:针对复合固体推进剂基体的大变形和界面的脱粘问题,对Mori-Tanaka法进行了改进.同时,为验证该方法的有效性,针对推进剂颗粒随机填充的特点,提出了一种含非线性界面脱粘的数值方法.最后以某推进剂配方为算例,对2种方法的计算结果进行了比较.结果表明,2种方法结果接近,从而验证了改进的Mori-Tanaka法的有效性,且...

关 键 词:复合固体推进剂  改进的Mori-Tanaka法  数值仿真  界面脱粘

An improved Mori-Tanaka method for nonlinear interface debonding in composite solid propellant
LIU Cheng-wu,YANG Jian-hong,CHEN Fei.An improved Mori-Tanaka method for nonlinear interface debonding in composite solid propellant[J].Journal of Solid Rocket Technology,2011,34(1):67-70.
Authors:LIU Cheng-wu  YANG Jian-hong  CHEN Fei
Institution:LIU Cheng-wu,YANG Jian-hong,CHEN Fei(Second Artillery Engineering College,Xi'an 710025,China)
Abstract:Aiming at the problems concerning the composite solid propellant with large deformation in the matrix and interface debonding around the filled particles,an improved Mori-Tanaka method was developed.At the same time,in order to verify its effectiveness,a simulation method for the interface debonding of the composite solid propellant consists of random filled particles was also put forward.Finally,a computational case of one kind of composite solid propellant was investigated.It is demonstrated that the resu...
Keywords:composite solid propellant  improved Mori-Tanaka method  numerical simulation  interface debonding  
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