| Citation: | LI Na, JI Hong-hu. Study on matching method for core and bypass mass flux of 2-D convergent nozzle of mixed flow[J]. Journal of Aerospace Power, 2011, 26(9): 2141-2147.
|
| [1] |
Martens R E.F-15 nozzle afterbody integration . AIAA-1974-1100,1974.
|
| [2] |
Richey G K,Berrier B L,Palcza J L.Two-dimensional nozzle-airframe integration technology:an overview . AIAA-1977-839,1977.
|
| [3] |
Berrier B L,Palcza J L,Richey G K.Nonaxisymmetric nozzle technology program:an overview .AIAA-1977-1225,1977.
|
| [4] |
Hiley P E,Wallace H W,Booz D E.Study of non-axisymmetric nozzles installed in advanced fighter aircraft .AIAA-1975-1316,1975.
|
| [5] |
Willard C M,Capone F J,Konarshi M,et al.Static performance of vectoring- reversing non-axisymmetric nozzles .AIAA-1977-840,1977.
|
| [6] |
Stevens H L.F-15/Nonaxisymmetric nozzle system integration study support program .NASA-CR-135252,1978.
|
| [7] |
Hinz W W,Miller E R.Propulsion integration of a supersonic strike-fighter .AIM Paper No.79-0100,1979.
|
| [8] |
Lander J A,Palcza J L.Exhaust nozzle deflector systems for V/STOL fighter aircraft .AIAA-1974-1169,1974.
|
| [9] |
Lander J A,Nash D O,Palcza J L.Augmented deflector exhaust nozzle/ADEN/design for future fighters .AIAA-1975-1318,1975.
|
| [10] |
Maiden D L.Performance of a isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 .NASA-TN D-8218,1976.
|
| [11] |
Maiden D L,Petit J E.Investigation of two-dimensional wedge exhaust nozzle for advanced aircraft[J].J.Aircraft,1976,13(10):809-816.
|
| [12] |
翟普,隋俊友,崔杰,等.弹用航空发动机尾喷流红外抑制技术研究[J].推进技术,1996,17(4):17-20. ZHAI Pu,SUI Junyou,CUI Jie,et al.A research on radiation restriction technique of a nozzle flow of aero-engine for missile[J].Journal of Propulsion Technology,1996,17(4):17-20.(in Chinese)
|
| [13] |
郑礼宝.二元喷管对发动机性能影响的实验研究[J].推进技术,1997,18(4):58-61. ZHENG Libao.Experimental investigation on the influence of 2-D nozzle on jet-engine performance[J].Journal of Propulsion Technology,1997,18(4):58-61.(in Chinese)
|
| [14] |
张勃.大宽高比矩形喷管的射流掺混与红外抑制特性研究 .南京:南京航空航天大学,2005. ZHANG Bo.Investigation of jet mixing characteristics and radiation restriction technology of rectangular nozzle with high aspect ratio .Nanjing:Nanjing University of Aeronautics and Astronautics,2005.(in Chinese)
|
| [15] |
罗明东.无人机排气系统红外隐身技术研究 .南京:南京航空航天大学,2006. LUO Mingdong.Investigation of infrared stealth technology of the exhaust system for unmanned Aerial vehicle .Nanjing:Nanjing University of Aeronautics and Astronautics,2006.(in Chinese)
|
| [16] |
陈玉春,黄兴,高本兵,等.发动机总体与尾喷管三维并行设计研究[J].航空动力学报,2007,22(10):1696-1699. CHEN Yuchun,HUANG Xing,GAO Benbing,et al.Parallel design of turbo engine and three-dimensional nozzle[J].Journal of Aerospace Power,2007,22(10):1696-1699. (in Chinese)
|
DownLoad: