[1]黄拳章,陈健,强洪夫,等.固体推进剂药柱局部夹杂应力场分析的边界元法[J].固体火箭技术,2019,42(03):275-281.
 HUANG Quanzhang,CHEN Jian,QIANG Hongfu,et al.Boundary element method for local stress field analysis of inclusions in solid propellant grain[J].Journal of Solid Rocket Technology,2019,42(03):275-281.
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固体推进剂药柱局部夹杂应力场分析的边界元法

参考文献/References:

[1]徐学文,孙建国,牟俊林.某固体火箭发动机药柱上三维裂纹扩展的判定[J].固体火箭技术,2008,31(4):331-335.XU Xuewen,SUN Jianguo,MU Junlin.Determination of 3D crack propagation for a solid rocket motor grain[J].Journal of Solid Rocket Technology,2008,31(4):331-335.[2]蒙上阳,唐国金,袁端才,等.含内聚空洞的固体火箭发动机药柱结构完整性分析[J].暨南大学学报,2005,26(1):64-68.MENG Shangyang,TANG Guojin,YUAN Duancai,et al.The structure integrity analysis of solid rocket motor grain with cohesive cavity[J].Journal of Jinan University(Natural Science),2005,26(1):64-68.[3]HAN B,JU Y T,ZHOU C S.Simulation of crack propagation in HTPB propellant using cohesive zone model[J].Engineering Failure Analysis,2012(26):304-317.[4]孙博,刘忠,朵英贤,等.含夹杂的固体火箭发动机药柱应变场分析[J].固体火箭技术,2016,39(2):174-178.SUN Bo,LIU Zhong,DUO Yingxian,et al.Strain field analysis of solid rocket motor grain with impurity[J].Journal of Solid Rocket Technology,2016,39(2):174-178.[5]Brebbia C A.The boundary element method in engineering practice[J].Engineering Analysis,1984,1(1):3-12. [6]蔡峨.粘弹性力学基础[M].北京:北京航空航天大学出版社,1989.CAI E.Foundation theory of viscoelasticity[M].Beijing:Beihang University Press,1989.[7]尚世英,李庆中.固体发动机药柱热线粘弹性边界元分析[J].推进技术,1993(2):57-62.SHANG Shiying,LI Qingzhong.Boundary element analysis of hot-linear viscoelasticity for solid motor grain[J].Journal of Propulsion Technology,1993(2):57-62.[8]黄拳章,郑小平,姚振汉.含液多孔固体的边界元方法及其等效力学性质模拟[J].清华大学学报(自然科学版),2011,51(4):471-477.HUANG Q Z,ZHENG X P,YAO Z H.Simulation of effective elastic properties of solids with fluid-filled pores using boundary element method[J].Tsinghua Science and Technology,2011,51(4):471-477.[9]HUANG Q Z,ZHENG X P,YAO Z H.Boundary element method for 2D solid with fluid-filled pores[J].Engineering Analysis with Boundary Elements,2011,35(2):191-199.[10]朱祖念.药柱结构完整性分析[M]//陈汝训.固体火箭发动机设计与研究(上).北京:宇航出版社,1991.ZHU Zunian.Structural integrity analysis of grain[M]//CHEN Ruxun.Study and design of solid rocket motor(Volume I).Beijing:China Astronautic Publishing House,1991.[11]傅学金.固体火箭发动机药柱燃烧过程应力应变有限元数值仿真[D].西安:第二炮兵工程学院,2004.FU Xuejin.Finite element simulation of stress and strain in solid rocket motor grain during combustion process[D].Xian:Second Artillery Engineering College,2004.

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