| Citation: | TANG Zheng-fu, ZHANG Jing-zhou, SHAN Yong. Effect of relative space between mixing duct exits on the flow temperature[J]. Journal of Aerospace Power, 2008, 23(7): 1194-1197. |
| [1] |
Armand F,Amelio Y.Infrared suppression for a gas turbine engine:US.Patent 5699955[P].1997.
|
| [2] |
Mark H,Walter M.Exhaust nozzle for suppressing infrared radiation:US,Patent 5992140[P].1999.
|
| [3] |
张靖周,李立国,高潮.直升机排气系统红外抑制器的模型实验研究[J].红外与毫米波学报,2005,24(2):125-129.ZHANG Jingzhou,LI Liguo,GAO Chao.Model experiments of infrared suppressor for helicopter exhaust system[J].Journal of Infrared and Millimeter Waves,2005,24(2):125-129.(in Chinese)
|
| [4] |
Kanclebo S W.Boeing silorsky findings underscore RAH-66 stealth[R].AW and ST,1993,22-23.
|
| [5] |
王先炜,黄勇,路玉霞.旋翼下洗气流对红外抑制器性能的影响研究[J].航空动力学报,2003,18(6):773-776.WANG Xianwei,HUANG Yong,LU Yuxia.Influences of the downwash flow from a helicopter rotor on the performances of an infrared suppressor[J].Journal of Aerospace Power,2003,18(6):773-776.(in Chinese)
|
| [6] |
唐正府,张靖周.波瓣喷管-狭长出口弯曲混合管引射混合特性分析[J],航空动力学报,2005,20(6);978-982.TANG Zhengfu,ZHANG Jingzhou.Investigation on ejecting and mixing characteristics of lobed nozzle with curved mixing duct and slot exit[J].Journal of Aerospace Power,2005,20(6):978-982.(in Chinese)
|
| [7] |
唐正府.张靖周.排气系统与机身一体化红外抑制器实验分析[J].航空动力学报,2007,22(2):233-237.TANG Zhengfu,ZHANG Jingzhou.Experimental research on infrared suppressor integrating the exhaust system with the tail part of a helicopter[J].Journal of Aerospace Power,2007,22(2):233-237.(in Chinese)
|
| [8] |
单勇,张靖周.渡瓣喷管引射-混合器的数值研究与验证[J].推进技术,2004,25(4):320-324.SHAN Yong,ZHANG Jingzhou.Numerical computation and examination of a lobed mixer-ejector[J].Journal of Propulsion Technology,2004,25(4):320-324.(in Chinese)
|