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2017年4月 固体火箭技术 第40卷 Part b,2009,40(6):483-494 2015,36(6):940-946. [32]陈广南,张为华固体火箭发动机撞击与热安全性分析[48] Zhou Jian- ping. A constitutive model of polymer materials in [M].北京:国防工业出版社,2008 cluding chemical ageing and mechanical damage and its ex [33 Rachael L Boddy, Peter J Gould, Andrew P Jardine. Damage verification[J]. Polymer, 1993, 34(20): 4252. in polymer bonded energetic composites: effect of loading rate[J].J. Dynamic Behavior Mater, 2016, 2(1): 157-165. [49] Herve H Trumel, Andre H Dragonl, Alain Fanget, et al.A [34] Drodge D R, Williamson D M Understanding damage in pol constitutive model for the dynamic and high-pressure behav ymer-bonded explosive composites [J].J Mater. Sci., 2016 iour of a propellant-like material: Part 1: Experimental back- 51(2):668-679 ground and general structure of the model[ J].Int J Numer. [35] Cornish R, Porter D, Church P, et al. Comparison of porter- Anal. Meth. Geomech., 2001, 25(6): 551-579 gould constitutive model with compression test data for HT- [50] Xu F, Aravas N, Sofronis P Constitutive modeling of solid PB/SUGAR[C]//AIP Conf. Proc., 2007, 955(1): 777-780. [36]刘著卿,李高春,邢耀国,等复合固体推进剂细观损伤 [J]Journal of the Mechanics and Physics of Solids, 200 扫描电镜实验及数值模拟[J].推进技术,2011,36(3) 412-416 [51] Yuna Kyeong-soo, Parkb Jae-beom, Jung Gyoo-dong Viscoe- [37]职世君,孙冰,张建伟固体推进剂复合型裂纹扩展数值 lastic constitutive modeling of solid propellant with damage 计算[J]固体火箭技术,2011,34(2):28-31 [JJ. International Journal of Solids and Structures, 2016, 80 38]徐学文,邢耀国,彭军固体火箭发动机装药裂纹危险性 (10):118-127 研究综述[J]海军航空工程学院学报,2007,2(1):101-[52]龚建良,刘佩进,李强基于能量守恒的复合固体推进剂 粘弹性本构关系[J]固体火箭技术,2013,36(4):529 [39] Abdelaziz M N, Neviere R, Pluvinage G Experimental meth- od for JIC computation on fracture of solid propellants under[53]王蓬勃,王政时,鞠玉涛,等双基推进剂高应变率型本 dynamic loading conditions[ J]. Engineering Fracture Me- 构模型的实验研究[J]固体火箭技术,2012,35(1):69 chanics,1987,28(4):425-434 72. 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Temperature dependence of high strain- (5):507-512. rate impact fracture behaviour in highly filled polymeric[56】王礼立,董新龙,孙紫建高应变率下计及损伤演化的材 composite and plasticized thermoplastic propellants [J] 料动态本构行为[J]爆炸与冲击,2006,26(3):193-198 Journal of Material Science, 1987, 22(8): 3023-3031 [57]王哲君,强洪夫,王广中应变率下HTPB推进剂压缩力 [42] Ho S Y, Fong C W Correlation between fracture propertie 学性能和本构模型研究[J]推进技术,2016,37(4):776- and dynamic mechanical relaxations in composite propel 782. ants[J] Polymer,1987,28(5):739-744 [58]冯震宙,王新军,王富生朱-王-唐非线性粘弹性本构模 [43]黄风雷,王泽平,丁敬复合固体推进剂动态断裂研究 型在有限元分析中的实现及其应用[J]材料科学与工 [J冂].兵工学报,1995,5(2):47-50 程学报,2007,25(2):269-272 [44]罗景润PBX的损伤断裂及本构关系研究[D]绵阳:中[59] Yang M, Shim v p w, Lim Ct.A visco- hyperelastic ap- 工程物理研究院,2001. proach to modelling the constitutive behaviour of rubber[J] [45]陈荣.一种PBX炸药试样在复杂应力动态加载下的力学 International Journal of Impact Engineering, 2000, 24(1) 性能实验研究[D].长沙:国防科学技术大学,2010. 545-560 [46]龙兵,常新龙,张有宏,等高应变率下HTPB推进剂动态[60]王哲君低温动态加载下HTPB推进剂力学行为的实验 端裂性能研究[J].推进技术,2015,36(3):471-475 和理论研究[D]西安:火箭军工程大学,2016 [47]郑健,汪文强,陈雄,等基于微观结构分析的CMDB推 (编辑:崔贤彬) 进剂动态断裂韧性加载率敏感性研究[J]推进技术, 182Part B,2009,40(6):483⁃494. [32] 陈广南,张为华.固体火箭发动机撞击与热安全性分析 [M].北京:国防工业出版社,2008. [33] Rachael L Boddy, Peter J Gould,Andrew P Jardine.Damage in polymer bonded energetic composites: effect of loading rate[J].J.Dynamic Behavior Mater.,2016,2(1):157⁃165. [34] Drodge D R,Williamson D M.Understanding damage in pol⁃ ymer⁃bonded explosive composites[ J].J. Mater. Sci.,2016, 51(2):668⁃679. [35] Cornish R,Porter D,Church P,et al.Comparison of porter⁃ gould constitutive model with compression test data for HT⁃ PB/ SUGAR[C] / / AIP Conf.Proc.,2007,955(1):777⁃780. [36] 刘著卿,李高春,邢耀国,等.复合固体推进剂细观损伤 扫描电镜实验及数值模拟[ J].推进技术,2011,36(3): 412⁃416. [37] 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,2011,34(2):28⁃31. [38] 徐学文,邢耀国,彭军.固体火箭发动机装药裂纹危险性 研究综述[J].海军航空工程学院学报,2007,22(1):101⁃ 105. [39] Abdelaziz M N,Neviere R,Pluvinage G.Experimental meth⁃ od for JIC computation on fracture of solid propellants under dynamic loading conditions [ J]. Engineering Fracture Me⁃ chanics,1987,28(4):425⁃434. 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