[1] |
刘大响, 金捷, 彭友梅, 等.大型飞机的发展现状和关键技术分析[J].航空动力学报, 2008, 23(6):976-980. LIU Daxiang, JIN Jie, PENG Youmei, et al.Summarization of development status and key technologies for large airplane engines[J].Journal of Aerospace Power, 2008, 23(6):976-980.(in Chinese)
|
[2] |
赵坚行.民用发动机污染排放及低污染燃烧技术发展趋势[J].航空动力学报, 2008, 23(6):986-996. ZHAO Jianxing.Pollutant emission and development of low-emission combustion technology for civil aero-engine[J].Journal of Aerospace Power, 2008, 23(6):986-996.(in Chinese)
|
[3] |
彭云晖, 许全宏, 张驰, 等.我国大飞机发动机低污染燃烧室发展考虑[C]//中国航空学会2007年学术年会动力专题论文集0701-04-54.深圳:中国航空学会动力分会, 2007:69.
|
[4] |
尚守堂, 程明, 张军峰, 等.低排放长寿命燃烧室关键技术分析[C]//中国航空学会2007年学术年会动力专题论文集0701-04-58.深圳:中国航空学会动力分会, 2007:70.
|
[5] |
彭云晖, 林宇震, 许全宏, 等.双旋流空气雾化喷嘴喷雾、流动和燃烧性能[J].航空学报, 2008, 29(1):1-14. PENG Yunhui, LIN Yuzhen, XU Quanhong, et al.Atomization, aerodynamics and combustion performance of swirl cup[J].Acta Aeronautica et Astronautica Sinica, 2008, 29(1):1-14.(in Chinese)
|
[6] |
Ateshkadi A, McDonell V G, Samuelsen G S.Effect of mixer geometry on fuel spray distribution, emission and stability[R].AIAA-98-0247, 1998.
|
[7] |
Wang H Y, McDonell V G, Sowa W A, et al.Scaling of the two phase flow downstream of a gas turbine combustor swirl cup:Part Ⅰ mean quantities[J].Journal of Engineering for Gas Turbines and Power, 1993, 115(3):453-460.
|
[8] |
Wang H Y, McDonell V G, Samuelsen G S.Influence of hardware design on the flow field structures and the patterns of droplet dispersion:Part Ⅰ mean quantities[J].Journal of Engineering for Gas Turbines and Power, 1995, 117(2):282-289.
|
[9] |
Wang H Y, McDonell V G, Samuelsen G S.The influence of spray angle on the continuous and discrete phase flow field downstream of an engine combustor swirl cup[R].AIAA-92-3231, 1992.
|
[10] |
Wang H Y, McDonell V G, Samuelsen G S.Correlation on droplet behavior with gas-phase structures in a gas turbine combustor[R].AIAA-93-1767, 1993.
|
[11] |
林宇震, 刘高恩, 王华芳.反向与同向双旋流器流场的实验研究[J].航空动力学报, 1995, 10(4):423-425. LIN Yuzhen, LIU Gaoen, WANG Huafang.An investigation of air flow field produced by a double-swirler airblast atomizer[J].Journal of Aerospace Power, 1995, 10(4):423-425.(in Chinese)
|
[12] |
张弛, 张荣伟, 徐国强, 等.直射式双旋流空气雾化喷嘴的雾化效果[J].航空动力学报, 2006, 21(5):805-809. ZHANG Chi, ZHANG Rongwei, XU Guoqiang, et al.Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup[J].Journal of Aerospace Power, 2006, 21(5):805-809.(in Chinese)
|
[13] |
Bulzan D L.Velocity and drop size measurements in a confined, swirler-stabilized, combusting spray[R].AIAA-96-3164, 1996.
|
[14] |
邢小军, 徐行, 郭志辉, 等.模型燃烧室冷态喷雾场实验研究[J].推进技术, 2000, 21(5):61-65. XING Xiaojun, XU Hang, GUO Zhihui.Experimental study on spray field in combustor by phase dopplor analyzer[J].Journal of Propulsion Technology, 2000, 21(5):61-65.(in Chinese)
|
[15] |
杨淑莹.VC++图像处理程序设计[M].北京:清华大学出版社, 2005.
|