[1]申柳雷,李海阳,申志彬.基于粘弹性VCFEM的复合固体推进剂等效松弛模量预示方法研究[J].固体火箭技术,2019,42(03):365-371.
 SHEN Liulei,LI Haiyang,SHEN Zhibin.Predication method of effective relaxation modulus of composite solid propellants based on viscoelastic VCFEM[J].Journal of Solid Rocket Technology,2019,42(03):365-371.
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基于粘弹性VCFEM的复合固体推进剂等效松弛模量预示方法研究

参考文献/References:

[1]彭威,任均国,周建平.复合推进剂粘弹性本构方程的细观力学分析(Ⅰ)球形颗粒增强效应分析[J].推进剂技术,1999,20(6):96-99.PENG Wei,REN Junguo,ZHOU Jianping.Micromechanics analysis on the viscoelastics constitutive law of composite sol id propellent (Ⅰ):reinforce effects of non-spherical particles[J].Journal of Propulsion Technology,1999,20(6):96-99.[2]彭威,任均国,周建平.复合推进剂粘弹性本构方程的细观力学分析(Ⅱ)非球颗粒增强效应分析[J].推进技术,2000,21(1):75-78.[JP2]PENG Wei ,REN Junguo,ZHOU Jianping.Micromechanics analysis on the viscoelastics constitutive law of composite sol id propellent (Ⅱ):reinforce effects of non-spherical particles[J].Journal of Propulsion Technology,2000,21(1):75-78.[3]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,2007,28(4):441-444.LI Gaochun ,XING Yaoguo,WANG Yufeng,et al.A micromechanicalmethod of the effectivemodulus estmiation for the composite propellant.Journal of Propulsion Technology,2007,28(4):441-444.[4]赵玖玲,强洪夫.MAPO含量和AP 级配对丁羟推进剂力学性能的影响[J].固体火箭技术,2011,34(3):329-334.ZHAO Jiuling,QIANG Hongfu.Effects of MAPO contents and AP size distribution on mechanical behavior of HTPB propellant[J].Journal of Solid Rocket Technology,2011,34(3):329-334. [5]张建伟,职世君,孙冰.基于细观颗粒夹杂模型的复合固体推进剂松弛模量预测[J].航空动力学报,2013,28(10):2370-2375.ZHANG Jianwei,ZHI Shijun,SUN Bing.Estimation of relaxation modulus of composite soid propellant based on particle packing mode[J].Journal of Aerospace Power,2013,28(10):2370-2375.[6]Ghosh S,Mukhopadhyay S N.A material based finite element analysis of heterogeneous media involving Dirichlet tessellations[J].Computer Methods in Applied Mechanics and Engineering,1993,104:211-247.[7]Guo R,Shi H J,Yao Z H.Modeling of interfacial debonding crack in particle reinforcedcomposites using Voronoi cell finite element method[J].Computational Mechanics,2003,32(1):52-59.[8]Zhang R,Guo R.Determination of crack tip stress intensity factors by singular Voronoi cell finite element model[J].Engineering Fracture Mechanics,2018,197:206-216.[9]郑宁昆.一个求解粘弹性夹杂问题的时域自适应Voronooi算法[D].大连:大连理工大学,2011.ZHENG Ningkun.An adaptive Voronoi algorithm in time domain for viscoelastic inclusion problem[D].Dalian:Dalian University of Technology,2011.[10]Shen L,Shen Z,Li H,et al. A Voronoi cell finite element method for estimating effective mechanical properties of composite solid propellants[J].Journal of Mechanical Science and Technology,2017,31(11):5377-5385. [11]Shen L,Shen Z,Li H.Effective mechanical property estimation of composite solid propellants based on VCFEM[J].International Journal of Aerospace Engineeing,2018,2018(2):1-9.[12]Shen L,Shen Z,Cui H,et al.Effect analysis of Interacial transition zone on basic mechanical properties of a composite solid propellant[J].Strength of Materials,2018,50(5):807-817.[13]GJB 770B—2005.火药试验方法[S].国防科工委军标出版发行部,2005.GJB 770B—2005,Test method of propellant[S].Commission of Science Technology and Industry of National Defense,2005.

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更新日期/Last Update: 2019-07-11
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