• 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