| Citation: | FANG Xin-xin, SHEN Chi-bing, ZHANG Xin-qiao. Experiment of breakup characteristics on conical sheets of pintle injectors[J]. Journal of Aerospace Power, 2016, 31(12): 3004-3009. doi: 10.13224/j.cnki.jasp.2016.12.024 |
| [1] |
张育林.变推力液体火箭发动机及其控制技术[M].北京:国防工业出版社,2001.
|
| [2] |
Dressler G A,Bauer J M.TRW pintle engine heritage and performance characteristics[R].AIAA-2000-3871,2000.
|
| [3] |
Dressier G,Stoddard F,Gavitt K.Test results from a simple,low-cost,pressure-fed liquid hydrogen/liquid oxygen rocket combustor[C]//Proceedings of 1993 JANNAF Propulsion Meeting.Monterey,US:Chemical Propulsion Information Agency,1993:51-67.
|
| [4] |
Hodge K F,Crofoot T A,Nelson S.Gelled propellants for tactical missile applications[R].AIAA 96-2869,1996.
|
| [5] |
Henneberry J P,Stoddard F J,Gu A L,et al.Low-cost expendable launch vehicles[R].AIAA 92-48990,1992.
|
| [6] |
Sackheim R L,Stoddard F J,Hardgrove J A.Propulsion advancements to lower the cost of satellite based communications systems[R].AIAA 94-0930,1994.
|
| [7] |
Fritz D,Dressler G,Mayer N,et al.Development and flight qualification of the propulsion and reaction control system for ERIS[R].AIAA 92-3663,1992.
|
| [8] |
Fritz D,Gavitt K.Gel propulsion for the fourth generation escape system component evaluation results[C]//Proceedings of 32nd Annual Symposium.Reno:SAFE Association,1994:371-378.
|
| [9] |
Gavitt K,Mueller T.TRW LCPE 650 klbf LOX/LH2 test results[R].AIAA-2000-3853,2000.
|
| [10] |
陈运钦.变流量喷注器的设计和性能试验[J].推进技术,1988,9(4):1-6,75. CHEN Yunqin.Design and functional test of controllable flow injector[J].Journal of Propulsion Technology,1988,9(4):1-6,75.(in Chinese)
|
| [11] |
岳春国,李进贤,冯喜平,等.针栓式变推力火箭发动机技术现状与发展探索[J].世界科技研究与发展,2008,30(5):609-612. YUE Chunguo,LI Jinxian,FENG Xiping,et al.The research on technology actuality and development of pintle injector variable thrust rocket engine[J].World Sci-Tech R&D,2008,30(5):609-612.(in Chinese)
|
| [12] |
张育林.变推力液体火箭发动机动态特性的状态空间分析[J].国防科技大学学报,1983(3):23-37. ZHANG Yulin.State-space analysis of the dynamic characteristics of a variable thrust liquid propellant rocket engine[J].Journal of National University of Defense Technology,1983(3):23-37.(in Chinese)
|
| [13] |
Marchi A,Nouri J,Yan Y,et al.Spray stability of outwards opening pintle injectors for stratified direct injection spark ignition engine operation[J].International Journal of Engine Research,2010,11(6):413-437.
|
| [14] |
Nouri J M,Hamid M A,Yan Y,et al.Spray characterization of a piezo pintle-type injector for gasoline direct injection engines[J].Journal of Physics:Conference Series,2007,85(1):281-292.
|
| [15] |
DONG Quan,Ishima T,Kawashima H.A study on the spray characteristics of a piezo pintle-type injector for DI gasoline engines[J].Journal of Mechanical Science and Technology,2013,27(7):1981-1993.
|
| [16] |
Son M,Yu K,Koo J,et al.Effects of momentum ratio andWeber number on spray half angles of liquid controlled pintle injector[J].Journal of Thermal Science,2015,24(1):37-43.
|
| [17] |
Gavaises M,Toninil S,Marchi1 A.Modelling of internal and near-nozzle flow of a pintle-type outwards-opening gasoline piezo-injector[J].International Journal of Engine Research,2006,7(5):381-397.
|
| [18] |
Nouri J M,Abo-Serie E,Marchi A,et al.Internal and near nozzle flow characteristics in an enlarged model of an outwards opening pintle-type gasoline injector[J].Journal of Physics:Conference Series,2007,85(1):256-267.
|
| [19] |
Kim D,Han P,Im J H,et al.Effect of recess on the spray characteristics of liquid-liquid swirl coaxial injectors[J].Journal of Propulsion and Power,2007,23(6):1194-1204.
|
| [20] |
Yang L J,Fu Q F,Qu Y Y,et al.Spray characteristics of gelled propellants in swirl injectors[J].Fuel,2012,97(7):253-261.
|
| [21] |
刘娟.旋转锥形液膜破碎过程实验与仿真研究[D].长沙:国防科学技术大学,2012. LIU Juan.Experimental and numerical simulation of the breakup process of swirling conical liquid sheet[D].Changsha:National University of Defense Technology,2012.(in Chinese)
|
| [22] |
富庆飞.液体火箭发动机同轴喷嘴稳/动态特性分析[D].北京:北京航空航天大学,2013. FU Qingfei.Investigation of the steady/dynamic characteristics of the coaxial injectors in liquid rocket engine[D].Beijing:Beijing University of Aeronautics and Astronautics,2013.(in Chinese)
|
| [23] |
何志勇,孙立宁,陈立国.Otsu准则下分割阈值的快速计算[J].电子学报,2013,41(2):267-272. HE Zhiyong,SUN Lining,CHEN Liguo.Fast computation of threshold based on Otsu criterion[J].Acta Electronica Sinica,2013,41(2):267-272.(in Chinese)
|
| [24] |
李继保,岳明,杨茂林.锥形液膜Kevin-Helmholtz波不稳定性的试验研究[J].航空动力学报,2007,22(3):337-341. LI Jibao,YUE Ming,YANG Maolin.Experimental research of instability of Kevin-Helmholtz wave on conical sheets[J].Journal of Aerospace Power,2007,22(3):337-341.(in Chinese)
|