[1]那旭东,夏智勋,马立坤,等.长时间小过载情况下固体火箭发动机两相流流场数值模拟[J].固体火箭技术,2018,41(06):694-701.
 NA Xudong,XIA Zhixun,MA Likun,et al.Numerical simulation of two -phase flow field under low acceleration with long operation time conditions for solid rocket motor[J].Journal of Solid Rocket Technology,2018,41(06):694-701.
点击复制

长时间小过载情况下固体火箭发动机两相流流场数值模拟

参考文献/References:

[1]许团委,田维平,王建儒,等.固体发动机地面过载试验凝相粒子加速度分析 [J].固体火箭技术,2014,37(4): 486-489.XU Tuanwei,TIAN Weiping,WANG Jianru,et al.Condensed phase particle acceleration analysis for overload test ground of solid rocket motor[J].Journal of Solid Rocket Technology,2014,37(4): 486-489.

[2]银美秀,黄家骥,陆明.过载条件下的火箭发动机工作状态研究 [J].品牌(市场研),2015(12): 117-117.YIN Meixiu,HUANG Jiaji,LU Ming.Research on rocket engine working condition under overload condition[J].Brand (market research),2015(12): 117-117.
[3]魏志军,张平,方蜀州.爱国者“PAC-3”型导弹主发动机装药药型反设计[J].固体火箭技术,2004,27(2): 114-116.WEI Zhijun,ZHANG Ping,FANG Shuzhou.Analysis on the grain design of the solid rocket motor for PATRIOT PAC-3 missile[J].Journal of Solid Rocket Technology,2004,27(2): 114-116.
[4]侯晓,付鹏,武渊.固体火箭发动机能量管理技术及其新进展 [J]. 固体火箭技术,2017,40(1): 1-6.HOU Xiao,FU Peng,WU Yuan.Energy management technology of SRM and its development[J].Journal of Solid Rocket Technology,2017,40(1): 1-6.
[5]曹军,郭颜红,邢强.高过载条件下固体火箭发动机工作稳定性研究[J].航空兵器,2014(1): 33-36.CAO Jun,GUO Yanhong,XING Qiang.Research on the working stabilization of solid rocket motor under high overload[J].Aero Weaponry,2014(1): 33-36.
[6]Sabnis J S,Jong F J D,Gibeling H J.Calculation of particle trajectories in solid-rocket motors with arbitrary celeration[J].Journal of Propulsion and Power,1992,8(5): 961-967.
[7]王国辉,何国强,刘佩进,等.过载状态下固体火箭发动机燃烧室内二相流动数值模拟[J].固体火箭技术,2001,24 (2): 8-12.WANG Guohui,HE Guoqiang,LIU Peijin,et al.Numerical simulation of two-phase flow in solid rocket motor combustion chamber under overload regime[J].Journal of Solid Rocket Technology,2001,24 (2): 8-12.
[8]何国强,王国辉,蔡体敏,等.高过载条件下固体发动机内流场及绝热层冲蚀研究[J].固体火箭技术,2001,24(4): 4-8.HE Guoqiang,,WANG Guohui,,CAI Timin,et al.Investigation on internal flow and insulator erosion of SRM under high acceleration[J].Journal of Solid Rocket Technology,2001,24(4): 4-8.
[9]刘洋.高过载固体发动机内流场模拟试验技术[D].西安:西北工业大学,2004.LIU Yang.The experimental simulation technique of flow field under high acceleration condition[D].Xi’an: Northwestern Polytechnical University,2004.
[10]乐发仁,冯喜平,武渊,等.高过载条件下固体火箭发动机绝热层失效研究[J].固体火箭技术,2005,28 (1): 33-35.YUE Faren,FENG Xiping,WU Yuan,et al.Investigation on abnormal insulator erosion under high flight acceleration load[J].Journal of Solid Rocket Technology,2005,28 (1): 33-35.
[11]李桢.横向过载下固体火箭发动机工作过程研究[D].长沙:国防科技大学,2005.LI Zhen.Investigation of the work process of solid rocket motor under lateral overload[D].Changsha: National University of Defense Technology,2005.
[12]刘洋,何国强,李江,等.过载条件下长尾喷管发动机三维两相流场数值研究[J].弹箭与制导学报,2006,26 (s2): 421-424.LIU Yang,HE Guoqiang,LI Jiang,et al.Numerical study on 3D twophase flow field for tail-pipe nozzle SRM under high celeration[J].Journal of Projectiles,Rockets,Missiles and Guidance,2006,26 (s2): 421-424.
[13]郭颜红,梁晓庚,陈斌.大过载下固体火箭发动机工作过程仿真的数学模型[J].航空兵器,2008(1): 21-25.GUO Yanhong,LIANG Xiaogeng,CHEN Bin.Working process simulation of solid rocket motor with high acceleration load[J].Aero aponry,2008(1): 21-25.
[14]李越森,叶定友.高过载下固体发动机内Al2O3粒子运动状况的数值模拟[J].固体火箭技术,2008,31(1): 24-27.LI Yuesen,YE Dingyou.Numerical simulation on movement of Al2O3 particles in solid motor under high overload[J].Journal of Solid Rocket Technology,2008,31(1): 24-27.
[15]高峰,王建辉,马岑睿.高过载下固体火箭发动机长尾喷管两相流场数值模拟[J].空军工程大学学报(自然科学版),2012,13(1): 1-5.GAO Feng,WANG Jianhui,MA Cenrui.Numerical simulation of the tail nozzle pipe of heat transfer in high acceleration[J].Journal of Air Force Engneering University( Natural Science Edition),2012,13(1): 1-5.
[16]邢志浩,刘燕宾,王虎干,等.过载条件下固体火箭发动机内流场及绝热层烧蚀研究[J].航空兵器,2013,(4): 37-40.XING Zhihao,LIU Yanbin,WANG Hugan,et al.Investigation on internal flow and insulator erosion of SRM under overload[J].Aero onry,2013(4): 37-40.
[17]何国强,王国辉,蔡体敏,等.过载条件下固体发动机内流场数值模拟[J].推进技术,2002,23(3): 182-185.HE Guoqiang,WANG Guohui,CAI Timin,et al.Numerical simulation on 3-D two phase flow field in SRM with acceleration load[J].Journal of Propulsion,2002,23(3): 182-185.
[18]刘长猛,余贞勇,李侃,等.飞行过载下燃烧室凝相粒子沉积特征数值研究[J]. 固体火箭技术,2017,40(3): 302-306.LIU Changmeng,YU Zhenyong,LI Kan,et al.Simulation research for accretion characteristic of condensed phase particle in SRM chamber with flight overload[J].Journal of Solid Rocket Technology,2017,40(3): 302-306.
[19]刘洋,吴育飞,李江,等.长时间小过载条件下发动机流场特征及绝热层烧蚀分析[J].推进技术,2013,34(8): 1071-1076.LIU Yang,WU Yufei,LI Jiang,et al.Flow field and ablation mode analysis of insulator under low acceleration with long operation time conditions for solid rocket motor[J].Journal of Solid Rocket Technology,2013,34(8): 1071-1076.
[20]许团委,田维平,王建儒.中、小过载下战术发动机内流场数值模拟[J].推进技术,2015,36(4): 532-539.XU Tuanwei,TIAN Weiping,WANG Jianru.Numerical simulation of flow field of tactical SRM with low and medium acceleration[J].Journal of Solid Rocket Technology,2015,36(4): 532-539.
[21]张宏安,叶定友,侯晓.固体火箭发动机凝聚相微粒分布研究现状[J].固体火箭技术,2000,23(3): 25-28.ZHANG Hongan,YE Dingyou,HOU Xiao.Recent status of research on condensedphase particles distribution in solid rocket motor[J].Journal of Solid Rocket Technology,2000,23(3): 25-28.
[22]李强,甘晓松,刘佩进,等.大型固体发动机潜入式喷管背壁区域熔渣沉积数值模拟[J].固体火箭技术,2010,33(2): 148-151.LI Qiang,GAN Xiaosong,LIU Peijin,et al.Numerical simulation of slag accumulation for Submerged nozzle of large scale SRM[J].Journal of Solid Rocket Technology,2010,33(2): 148-151.
[23]刘洋,何国强,李江,等.聚集状态下凝相颗粒的收集与测量[J].推进技术,2005,26(5): 477-480.LIU Yang,HE Guoqiang,LI Jiang,et al.Collection and measurement condensed particle under aggregation condition[J].Journal of Solid Rocket Technology,2005,26(5): 477-480.
[24]李强,李江,刘佩进,等.模型发动机内凝相颗粒碰撞的数值模拟[J].推进技术,2008,29(1): 18-21.LI Qiang,LI Jiang,LIU Peijin,et al.Numerical simulation of particle collision and impingement for a model SRM[J].Journal of Propulsion Technology,2008,29(1): 18-21.
[25]Cortopassi A,Boyer E,Kuo K.Update: a subscale solid rocket motor for characterization of submerged nozzle erosion[C]//In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit,2-5 August 2009,Denver,Colorado.
[26]Houim R W.Modeling the influence of shock waves on the combustion of aluminum droplets[D].The Pennsylvania State University,2011.[27]夏盛勇.三氧化二铝液滴碰撞机理及模型研究[D].西安:西北工业大学,2015.XIA Shengyong.Physics and model of alumina droplet collisions[D].Xi’an:Northwestern Polytechnical University,2015.
[28]Mundo C,Sommerfeld M,Tropea C.Dropletwall collisions: Experimental studies of the deformation and breakup rocess[J].International Journal of Multiphase Flow,1995,21(2): 151-173.
[29]Mundo C,Tropea C,Sommerfeld M.Numerical and experimental investigation of spray characteristics in the vicinity of a rigid Wall[J].Experimental Thermal and Fluid Science,1997,15(3): 228-237.
[30]王德全,夏智勋,胡建新,等.铝镁贫氧推进剂固冲发动机沉积数值模拟[J].航空动力学报,2009,24(2):445-449.WANG Dequan,XIA Zhixun,HU Jianxin,et al.Numerical simulation of deposition for aluminum/magnesiumloaded fuelrich propellant ducted rockets[J].Journal of Aerospace Power,2009,24(2):445-449.
[31]关轶文,李江,刘洋,等.高温氧化铝液滴沉积条件下绝热材料烧蚀实验方法研究[J].推进技术,2017,38(6):1402-1408.GUAN Yiwen,LI Jiang,LIU Yang,et al.Experimental method research on ablation characteristic of insulation material under high temperature alumina droplet deposition condition[J].Journal of Propulsion Technology,2017,38(6): 1402-1408.
[32]张志峰,蔡体敏.旋转条件下固体火箭发动机三维内流场数值模拟[J].固体火箭技术,2007,30(4): 302-305.ZHANG Zhifeng,CAI Timin.Numerical simulation on 3D internal flow field of SRM under spinning condition[J].Journal of Solid Rocket Technology,2007,30(4): 302-305.
[33]苏鹏辉,艾邦成,潘宏禄.喷管两相流耦合数值模拟与粒子热增量预测[J].北京航空航天大学学报,2012,38(7): 900-904.SU Penghui,AI Bangcheng,PAN Honglu.Two-phase flow numerical simulation and particle impingement heating prediction in SRM zle[J].Journal of Beijing University of Aeronautics and Astronautics,2012,38(7): 900-904.

相似文献/References:

[1]李娟,李江,王毅林,等.喉栓式变推力发动机性能研究 [J].固体火箭技术,2007,(6):505.
[2]尤军峰,陈汝训.固体火箭发动机壳体后封头屈曲分析[J].固体火箭技术,2008,(2):173.
[3]陈林泉,毛根旺,张胜勇.高能固体火箭发动机爆炸冲击波毁伤效应研究[J].固体火箭技术,2008,(6):588.
[4]白宏伟,尤军峰,张铎,等.级间热分离条件下带有延伸喷管的固体火箭发动机尾部流场分析[J].固体火箭技术,2008,(6):595.
[5]陈林泉,毛根旺,陈军涛.采用高低燃温组合装药降低喷管内表面温度和烧蚀研究[J].固体火箭技术,2008,(6):599.
[6]苑博,刘勇琼,尤军峰,等.轴压载荷作用下全复合材料裙与壳体搭接区的结构分析[J].固体火箭技术,2008,(6):629.
[7]樊建龙,唐金兰,李进贤,等.固体火箭发动机点火瞬间火焰传播模型比较研究[J].固体火箭技术,2008,(6):575.
[8]窦毅芳,刘飞,张为华.基于张量积函数的固体火箭发动机性能散布分析[J].固体火箭技术,2008,(6):579.
[9]甘晓松,贾有军,鲁传敬,等.水下燃气射流流场数值研究[J].固体火箭技术,2009,(01):23.
[10]邹汝平,李晓斌,张为华.固体发动机内弹道计算不确定性研究[J].固体火箭技术,2009,(01):33.

更新日期/Last Update: 2019-01-02
分享