[1] Matous K,Inglis H M, Gu X F,et al.Multiscale Damage Modeling of Solid Propellants:Theory and Computational Framework[R].AIAA 2005-4347.
[2] Matous K, Geubelle P H.Multiscale Modeling of Particle Debonding in Reinforced Elastomers Subjected to Finite Deformation[J].International Journal for Numerical Methods in Engineering,6,5:190-223.
[3] Tan H, Liu C,Huang Y, et al.The Cohesive Law for the Particle/Matrix Interfaces in High Explosives[J].Journal of the Mechanics and Physics of Solids,5,3:1892-1917.
[4] Tan H, Huang Y,Liu C,et al.The Uniaxial Tension of Particulate Composite Materials with Nonlinear Interface Debonding[J].International Journal of Solids and Structures,7,4:1809-1822.
[5] 李高春, 邢耀国, 王玉峰,等.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.7,8(4):441-444.(LI Gao-chun,XING Yao-guo,WANG Yu-feng,et al.A Micromechanical Method of the Effective Modulus Estimation for the Composite Propellant[J].Journal of Propulsion Technology,7,8(4):441-444.)
[6] 曲凯, 张旭东, 李高春.基于内聚力界面脱粘的复合固体推进剂力学性能研究[J].火炸药学报,8,1(6):77-81.
[7] 马昌兵, 强洪夫, 武文明,等.颗粒增强复合材料有效弹性模量预测的多步法[J].固体力学学报,0,1:12-16.
[8] 李高春, 邢耀国, 戢治洪,等.复合固体推进剂细观界面脱粘有限元分析[J].复合材料学报,1,8(3):229-235.
[9] 刘承武, 阳建红, 陈飞.改进的Mori-Tanaka法在复合推进剂非线界面脱粘中的应用[J].固体火箭技术,1,4(1):67-70.
[10] Buckmaster J,Jackson T L, Ulrich M.Numerical Modeling of Heterogeneous Propellant Combustion[R]. AIAA 2001-3579.
[11] Knott G M,Jackson T L, Buckmaster J.Random Packing of Heterogeneous Propellants[J].AIAA Journal,1,9(4):678-686.
[12] 王勖成.有限元单元法 [M].北京:清华大学出版社, 2003.
[13] 职世君, 孙冰, 张建伟.固体推进剂复合型裂纹扩展数值计算[J].固体火箭技术,1,4(1):28-31.
[14] Liu C T.A Probabilistic Crack Growth Model for Application to Composite Solid Propellants[R].AIAA 91-0917.
|