DocumentCode :
3083175
Title :
Impact of the Angle of External Flow on the Performance of Counterflow Thrust Vectoring Nozzle
Author :
Liu Zhao-miao ; Chen Chuan
Author_Institution :
Coll. of Mech. Eng. & Appl. Electron., Beijing Univ. of Technol., Beijing, China
fYear :
2013
fDate :
21-23 July 2013
Firstpage :
52
Lastpage :
55
Abstract :
The performance and structure of the internal flow field of counterflow thrust vectoring nozzle under the impact of the external flow were studied by numerical simulation, considering the angle of external flow on the vectoring angle and the mass flux ratio of secondary flow. The results show that, when the external flow is of the same Mach number and the angle of the external flow increase in positive way, the vectoring angle will increase and the mass flux ratio of secondary flow will increase in forward flow direction. When the angle of the external flow increases in negative way, the vectoring angle will increase in backward flow direction.
Keywords :
Mach number; flux flow; nozzles; numerical analysis; Mach number; backward flow direction; counterflow thrust vectoring nozzle; external flow angle; forward flow direction; internal flow field; mass flux ratio; numerical simulation; secondary flow; vectoring angle; Aerodynamics; Computational modeling; Educational institutions; Force; Numerical models; Numerical simulation; Turbines; angle of external flow; counterflow thrust vectoring; impact of external flow;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechanical and Automation Engineering (MAEE), 2013 International Conference on
Conference_Location :
Jiujang
Type :
conf
DOI :
10.1109/MAEE.2013.23
Filename :
6602136
Link To Document :
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