[1] 果琳丽,王平,梁鲁,等. 载人月面着陆及起飞技术初步研究[J]. 航天返回与遥感,2013,34(4):10-16.GUO L L,WANG P,LIANG L,et al.Preliminary research on manned lunar landingand lifting off technology[J].Spacecraft Recovery & Remote Sensing,2013,34(4):10-16(in Chinese).
[2] CAPORICCI M. European crew and logistics vehicles for ISS and exploration missions:AIAA-2005-3252[R].Reston,VA:AIAA,2005.
[3] BENNETT F V.Apollo experience report:Mission planning for lunar module descent and ascent:NASA-TN-D-6846[R].Washington,D.C.:NASA,1972.
[4] EVANS R,SPARKS O.Launch deflector design criteria and their application to the SATURN C-1 deflector:NASA-TN-D-1275[R].Washington,D.C.:NASA,1963.
[5] TSUTSUMI S,KATO S,FUKUDA K,et al.Effect of deflector shape on acoustic field of launch vehicle at lift-off:AIAA-2009-0328[R].Reston,VA:AIAA,2009.
[6] SACHDEV J S,AHUJA V,HOSANGADI A,et al.Analysis of flame deflector spray nozzles in rocket engine test stands:AIAA-2010-6972[R].Reston,VA:AIAA,2010.
[7] ANOOP P, UNNIKRISHNAN C,SUNDAR B,et al.Thermal analysis of a jet deflector subjected to liquid engine jet exhaust in a static test[J].Heat Transfer Engineering,2015,36(4):346-351.
[8] OH H,LEE J,UM H,et al.Numerical study for flame deflector design of a space launch vehicle[J].Advances in Space Research,2017,59(7):1833-1847.
[9] 贺卫东.发动机真空羽流导流力热效应的CFD/DSMC耦合仿真及试验研究[D].北京:北京理工大学,2015.HE W D.Numerical simulation and experiment research on force and heat effect of vacuum plume with CFD&DSMC coupled method[D].Beijing:Beijing Institute of Technology,2015(in Chinese).
[10] 贺卫东,党海燕.CFD/DSMC耦合仿真方法在天基发射羽流导流技术研究中的应用[J].导弹与航天运载技术,2015(2):53-57.HE W D,DANG H Y.Application of CFD/DSMC coupling simulation method in the research of space-based launch plume diversion technique[J].Missiles and Space Vehicles,2015(2):53-57(in Chinese).
[11] 贺卫东,党海燕,鲁志刚,等.基于地外天体起飞的真空羽流导引技术研究方案评述[J].航天器环境工程,2015,32(2):206-210.HE W D,DANG H Y,LU Z G,et al.Review of the studies of vacuum plume diversion technique for probe taking off from celestial bodies outside the Earth[J].Spacecraft Environment Engineering,2015,32(2):206-210(in Chinese).
[12] 贺卫东,党海燕,许明艳,等.地外天体起飞过程真空羽流导流力热效应研究[J].推进技术,2015,36(8):1151-1156.HE W D,DANG H Y,XU M Y,et al.Research on impact and thermal effect of celestial takeoff vacuum exhaust plume[J].Journal of Propulsion Technology,2015,36(8):1151-1156(in Chinese).
[13] ZHANG M X,CAI G B,TANG Z Y,et al.Experimental and numerical research on the diversion effect of a conic flame deflector for a lunar module ascent stage[J].Journal of Aerospace Engineering,2016,29(5):04016021.
[14] 张萃,王刚,刘峰,等.着陆器顶板羽流导向设计及验证技术[J].航天返回与遥感,2016,37(2):34-41.ZHANG C,WANG G,LIU F,et al.Design and verification thechnology of plume guiding device on lander roof[J].Spacecraft Recovery & Remote Sensing,2016,37(2):34-41(in Chinese).
[15] 黄琳,陈伟芳,吴其芬,等.姿控发动机内流场及高空羽流流场的DSMC一体化数值模拟[J].空气动力学学报,2001,19(4):383-387.HUANG L,CHEN W F,WU Q F,et al.The overall numerical simulation of both high-altitude plume flowfield and inflow region with DSMC method[J].Acta Aerodynamica Sinica,2001,19(4):383-387(in Chinese).
[16] 程晓丽,李明智,毛铭芳,等.高空羽流场的DSMC计算和实验研究[J].空气动力学学报,2002,20(1):9-14.CHENG X L,LI M Z,MAO M F,et al.Experimental and numerical investigation of a high-altitude plume flow using DSMC method[J].Acta Aerodynamica Sinica,2002,20(1):9-14(in Chinese).
[17] 黄琳,聂万胜,陈伟芳.姿控发动机高空羽流流场干扰效应的DSMC方法研究[J].空气动力学学报,2003,21(1):104-108.HUANG L,NIE W S,CHEN W F.Studying of multi-plume interference effects for attitude-control thruster with DSMC method[J].Acta Aerodynamica Sinica,2003,21(1):104-108(in Chinese).
[18] 蔡国飙,贺碧蛟.PWS软件应用于探月着陆器羽流效应数值模拟研究[J].航天器环境工程,2010,27(1):18-23.CAI G B,HE B J.PWS software applied to numerical simulation on plume effect of lunar exploration lander[J].Spacecraft Environment Engineering,2010,27(1):18-23(in Chinese).
[19] 张熇,蔡国飙,许映乔,等.嫦娥三号着陆器软着陆过程中羽流仿真分析及试验研究[J].中国科学:技术科学,2014,44(4):344-352.ZHANG H,CAI G B,XU Y Q,et al.Simulation and experimental study of the plume during the Chang'E-3 lunar landing[J].Scientia Sinica Technologica,2014,44(4):344-352(in Chinese). |