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