| Citation: | MAO Xiao-fang, TANG Zhen-yu, CAI Guo-biao. Simulation on working process of 10N attitude-control thruster combustion chamber at lower-pressure condition[J]. Journal of Aerospace Power, 2013, 28(3): 550-555.
|
| [1] |
Webber W T,Hoffman R J.A mechanistic model for analysis of pulse-mode engine operation[R].AIAA 72-1184,1972.
|
| [2] |
Trinks H.Experimental exhaust plume analysis with MBB 10N thruster[R].AIAA 83-1259,1983.
|
| [3] |
Trinks H,Hoffman R J.Experimental investigation of bipropellant exhaust plume flowfield,heating,and contamination,and comparison with the CONTAM computer model predictions[R].AIAA 83-1447,1983.
|
| [4] |
Hoffman R J,Webber W T,Oeding R G.An analytical model for the prediction of liquid rocket plume contamination effects on sensitive surfaces[R].AIAA 72-1172,1972.
|
| [5] |
Preclik D,Estublier D.An Eulerian-Lagrangian approach to spray combustion modeling for liquid bi-propellant rocket motors[R].AIAA 95-2779,1995.
|
| [6] |
Knab O,Preclik D,Estublier D.Flow field prediction within liquid film cooled combustion chambers of storable bi-propellant rocket engines[R].AIAA 98-3370,1998.
|
| [7] |
庄逢辰.液体火箭发动机喷雾燃烧的理论、模型及应用[M].长沙:国防科技大学出版社,1995.
|
| [8] |
庄逢辰.计算机数值模拟与仿真在液体火箭发动机喷雾燃烧设计中的应用[J].指挥技术学院学报,2000,11(1):1-7. ZHUANG Fengchen.The applicatio of computer numerical modeling and simulation technology in liquid rocket engine spray combustion design[J].Journal of Institute of Command and Technology,2000,11(1):1-7.(in Chinese)
|
| [9] |
刘娟,潘余,刘卫东,等.超燃冲压发动机双凹腔燃烧室氢气燃烧流场分析[J].航空动力学报,2009,24(11): 2501-2505. LIU Juan,PAN Yu,LIU Weidong,et al.Analysis of the hydrogen combustion field in scramjet dual-cavity combustor[J].Journal of Aerospace Power,2009,24(11): 2501-2505.(in Chinese)
|
| [10] |
苏龙斐,张黎辉,潘海林.卫星推进系统发动机启动过程数值仿真[J].航空动力学报,2005,20(4):698-701. SU Longfei,ZHANG Lihui,PAN Hailin.Numerical simulation on the starting process of satellite propulsion system[J].Journal of Aerospace Power,2005,20(4):698-701.(in Chinese)
|
| [11] |
李丹琳,田原,孙纪国.隔板对燃烧室声学特性的影响[J].航空动力学报,2012,27(3): 715-720. LI Danlin,TIAN Yuan,SUN Jiguo.Effects of baffle on combustion acoustic characteristics of liquid rocket engine[J].Journal of Aerospace Power,2012,27(3): 715-720.(in Chinese)
|
| [12] |
Webber W T.Calculation of low-frequency [JP+1]unsteady behavior of liquid rockets from droplet combustion parameters[J].Journal of Spacecraft and Rockets,1972,9:231-237.
|
| [13] |
Agosta V D,Seamans T F,Vanpee M.Development of a fundamental model of hypergolic ignition in space-ambient engines[J].AIAA Jounal,1967,5:1616-1624.
|
| [14] |
唐振宇,侯凤龙,蔡国飙.双组元姿控发动机燃烧室瞬态工作过程仿真模型[J].推进技术,2012,33(4):193-197. TANG Zhenyu,HOU Fenglong,CAI Guobiao.A model for simulating the transient process for combustion chamber of bipropellant attitude-control engine[J].2012,33(4):193-197.(in Chinese)
|
| [15] |
李宜敏,张中钦,张远君.固体火箭发动机原理[M].北京:北京航空航天大学出版社,1999.
|
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