| Citation: | LUO Lian-jun, LIU Yu-ying, ZHANG Wen-long, JI He-ming. Atomization characteristics of fuel injector and cavity-based strut flame stabilizer under close-range matching condition[J]. Journal of Aerospace Power, 2013, 28(11): 2462-2467. |
| [1] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第11册 加力燃烧室[M].北京:航空工业出版社,2001.
|
| [2] |
侯晓春,季鹤鸣,刘庆国,等.高性能航空燃气轮机燃烧技术[M].北京:国防工业出版社,2002.
|
| [3] |
马梦颖,金捷,季鹤鸣.航空发动机加力燃烧室技术及新颖结构方案[J].燃气涡轮试验与研究,2008,21(4):55-59. MA Mengying,JIN Jie,JI Heming.Technology and new configuration of aero-engine afterburner[J].Gas Turbine Experiment and Research,2008,21(4):55-59.(in Chinese)
|
| [4] |
孙雨超,张志学,李江宁,等.一体化加力燃烧室方案设计及数值研究[J].航空科学技术,2011(4):71-74. SUN Yuchao,ZHANG Zhixue,LI Jiangning,et al.Design and numerical research of integrated rear frame and afterburner[J].Aeronautical Science and Technology,2011(4):71-74.(in Chinese)
|
| [5] |
金如山,索建秦.先进加力燃烧室技术发展.贵阳:中国航空学会第七届动力年会,2010.
|
| [6] |
季鹤鸣,樊未军,杨茂林.新型内突扩加力燃烧室方案可行性分析[J].航空发动机,2006,32(1):35-37. JI Heming,FAN Weijun,YANG Maolin. Feasibility analysis of a new inner dumped afterburner concept[J].Aeroengine,2006,32(1):35-37.(in Chinese)
|
| [7] |
吴迪,金捷,季鹤鸣.一种加力燃烧室凹腔支板火焰稳定方案研究.贵阳:中国航空学会第七届动力年会,2010.
|
| [8] |
吴迪,金捷,季鹤鸣,等.凹腔支板尾缘涡脱落频率试验研究[J].航空发动机,2011,37(4):48-51. WU Di,JIN Jie,JI Heming,et al.Experimental study of vortex shedding frequency at trailing edge of a cavity-based strut[J].Aeroengine,2011,7(4):48-51.(in Chinese)
|
| [9] |
吴迪.新型一体化加力燃烧室冷态流场试验研究.北京:北京航空航天大学,2010. WU Di.Experimental research of non-reacting flow fields in a novel integrated afterburner.Beijing:Beijing University of Aeronautics and Astronautics,2010.(in Chinese)
|
| [10] |
刘雯佳,金捷,季鹤鸣.带凹腔支板的数值模拟[J].燃气涡轮试验与研究,2010,23(4):35-38. LIU Wenjia,JIN Jie,JI Heming.Numerical simulation on strut with cavity[J].Gas Turbine Experiment and Research,2010,23(4):35-38.(in Chinese)
|
| [11] |
Lovett J A,Brogan T P,Philippon D S,et al.Development needs for advanced afterburner designs.AIAA-2004-4192,2004.
|
| [12] |
王俭,顾善建,杨茂林,等.直射式喷嘴跨流喷射的雾化特性实验研究[J].航空学报,1990,11(4):157-164. WANG Jian,GU Shanjian,YANG Maolin.Study on atomization features of a plain injector in high speed transverse air stream[J].Acta Aeronautica et Astronautica Sinica,1990,11(4):157-164.(in Chinese)
|
| [13] |
徐行,郭志辉,边寿华.直射式喷嘴喷雾特性的实验研究[J].航空动力学报,1997,12(4):341-344. XU Hang,GUO Zhihui,BIAN Shouhua.Experiment on spray characteristics of direct injector[J].Journal of Aerospace Power,1997,12(4):341-344.(in Chinese)
|
| [14] |
柳杨,马文杰,李瑞明,等.侧喷挡板式雾化喷油杆喷雾特性实验[J].航空动力学报,2009,24(5):987-993. LIU Yang,MA Wenjie,LI Ruiming,et al.Experiment on spray characteristics of baffle-type injector in cross flow[J].Journal of Aerospace Power,2009,24(5):987-993.(in Chinese)
|
| [15] |
杨茂林,黄勇,顾善建,等.燃油在稳定器尾缘的二次雾化研究[J].航空动力学报,1992,7(1):61-64. YANG Maolin,HUANG Yong,GU Shanjiang,et al.Study on secondary atomization of liquid fuel at the lip of the flameholder[J].Journal of Aerospace Power,1992,7(1):61-64.(in Chinese)
|