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[1]宋 戈,连军伟,丁振晓.用于PDPA校准的标准气溶胶发生器性能研究[J].火箭推进,2018,44(04):54-59.
 SONG Ge,LIAN Junwei,DING Zhenxiao.Performance study on standard aerosol generators for calibration of PDPA[J].Journal of Rocket Propulsion,2018,44(04):54-59.
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用于PDPA校准的标准气溶胶发生器性能研究

参考文献/References:

[1] POPE S B. Turbulent flows [M]. England: Cambridge University Press, 2000.
[2] 沈熊.激光多普勒测速技术及应用[M]. 北京: 清华大学出版社,2004.
[3] 程圣清, 宋连忠, 王珏. 氢氧火箭发动机预燃室喷注器特性研究[J]. 导弹与航天运载技术,1998(1):6-15.
[4] 黄兵, 张楠. 液体火箭发动机初始雾化液滴分布预测[J].火箭推进,2007,33(2):31-39.
HUANG Bing, ZHANG Nan. Prediction of droplet size distributions of primary atomization in liquid rocket engine [J]. Journal of rocket propulsion, 2007, 33(2): 31-39.
[5] 费俊.射流撞击雾化液滴运动过程与粒径分布特性的试验研究[J].火箭推进,2015,41(1):10-14.
FEI Jun. Experimental analysis on movement and size distribution of atomized droplets from impinging liquid jet [J]. Journal of rocket propulsion, 2015, 41(1): 10-14.
[6] 卢正永.气溶胶科学引论[M], 北京:原子能出版社,2000.
[7] 倪守邦. 国外气溶胶发生装置研制情况.冶金安全[J],1982(1):34-38.
[8] 杜斯特 F, 梅林A, 怀特洛J H.激光多普勒测速技术的原理和实践[M]. 北京:科学出版社,1992.
[9] 刘志军.高效空气过滤器测试用气溶胶发生器的研制及性能评价[D].天津:天津大学,2006.
[10] Thermo-Systems Incorporated(TSI). MDG-100 monosize droplet generator operation and service manual [M]. [S.l.]: TSI, 2006.
[11] Thermo-Systems Incorporated(TSI). Phase doppler particle analyzer(PDPA)laser Doppler velocimeter(LDV)operations manual [M]. [S.l.]: TSI, 2006.
[12] 沈熊等.应用激光相位-多普勒系统测量雾化液滴颗粒和流动特性[J].流体力学实验和测量,2000,14(2):54-60.
[13] 陈剑.应用激光相位多普勒技术对燃料喷雾特性的研究[D].上海:上海交通大学, 2004.
[14] 徐学哲, 赵卫雄, 方波, 等. 标准气溶胶发生系统的建立与性能评估[J].环境科学学报,2016.7(36):2355-2361.

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备注/Memo

收稿日期:2017-11-05
作者简介: 宋 戈(1987—),男,硕士,研究领域为液体火箭发动机流体试验技术及光学测量技术应用研究

更新日期/Last Update: 1900-01-01