[1]李鑫,李耿,王周成,等.超音速分离线喷管内流场数值模拟[J].固体火箭技术,2019,42(04):433-439.
 LI Xin,LI Geng,WANG Zhoucheng,et al.Numerical simulation of supersonic splitline nozzle flow field[J].Journal of Solid Rocket Technology,2019,42(04):433-439.
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超音速分离线喷管内流场数值模拟

参考文献/References:

[1]陈汝训.固体火箭发动机设计与研究[M].北京:宇航出版社,1991.CHEN Ruxun.Solid motor design and research[M].Beijing:China Astronautic Publishing House,1991.[2]Berdoyes M.Snecma propulsion solide advanced technology SRM nozzles history and future[C]//Sacramento,The 42nd AIAA/ ASME/ SAE/ ASEE Joint Propulsion Conference & Exhibit,2006.[3]Crapiz D.Improvements in composite tactical solid rocket motor technology[R].America Institute of Aeronautics and Astronautics,1990-1975.[4]Φrbekk D E.Novel TVC system utilizing guide vanes with jet flap’s into a high efficiency compact nozzle[R].America Institute of Aeronautics and Astronautics,2005-4499.[5]Φrbekk D E.Supersonic splitline TVC technology and testing at nammo raufoss AS[R].America Institute of Aeronautics and Astronautics, 2006-4940.[6]Larrieu J M,Ceccarelli A L.Supersonic splitline cold ball & socket nozzle(SSCBSN),a costeffective and compact thrust vector control solution for booster and cruise stages[C]//5th European Conference for Aeronautics and Space Science,2013. [7]Erland orbekk.Supersonic split line TVC technology and testing at nammo raufoss AS[C]//42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit,Sacramento,California,2006.[8]贺征,郜冶.星孔型装药发动机三维两相流场的数值模拟[J].推进技术,2004,25(2):118-121.HE Zheng,GAO Ye.Numerical simulation of 3-D two-phase flow in solid rocket motor with star grain[J].Journal of Propulsion Technology,2004,25(2):118-121.[9]杨丹.固体火箭发动机气固两相流的数值模拟[D].哈尔滨:哈尔滨工程大学,2006.YANG Dan.Numerical simulation of gas-partical flow in solid rocket motor[D].Harbin:Harbin Engineering University,2006.[10]于勇,刘淑艳,张世军,等.固体火箭发动机喷管气固两相流动的数值研究[J].航空动力学报,2009,24(4):931-937.YU Yong,LIU Shuyan,ZHANG Shijun,et al.Numerical simulation of gas-partical flow in nozzle of solid rocket motor[J].Journal of Aerospace Power,2009,24(4):931-937.[11]方丁酉.两相流动力学[M].长沙:国防科技大学出版社,1988.FANG Dingyou.Two-phase flow dynamics[M].Changsha:National University of Defense Technology Press,1988.[12]李江.固体火箭发动机凝相颗粒运动规律研究[D].西安:西北工业大学,1998.LI Jiang.A study of partical motion patterns in solid rocket motor[D].Xi’an:Northwestern Polytechnical University,1998. [13]淡林鹏,张振鹏,赵永忠,等.长尾喷管中粒子运动轨迹的数值模拟[J].航空动力学报,2003,18(2):197-202.DAN Linpeng,ZHANG Zhenpeng,ZHAO Yongzhong,et al.Numerical study of particle trajectories in a nozzle with a tail pipe[J].Journal of Aerospace Power,2003,18(2):197-202.[14]阎超.计算流体力学方法及应用[M].北京:北京航空航天大学出版社,2006.YAN Chao.Methods and application of computational fluid dynamics[M].Beijing:Beihang University Press,2006.[15]John D Anderson.计算流体力学入门[M].北京:清华大学出版社,2002.John D Anderson.Computational fluid dynamics the basics with applications[M].Beijing:Tsinghua University Press,2002.[16]武利敏.固体火箭发动机两相流计算模型分析与比较[D].哈尔滨:哈尔滨工程大学,2007.WU Limin.Contrast of numerical simulation models of twophase flow in solid rocket motor[D].Harbin:Harbin Engineering University,2007.[17]吴限德,张斌,陈卫东,等.固体火箭发动机喷管内气粒两相流动的CFD_DSMC模拟[J].固体火箭技术,2011,34(6):707-710.WU Xiande,ZHANG Bin,CHEN Weidong,et al.Numerical simulation of gasparticle twophase flow in SRM nozzle by the method of CFDDSMC[J].Journal of Solid Rocket Technology,2011,34(6):707-710.

更新日期/Last Update: 2019-08-29
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