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Research Progress of the Dual-throat Thrust-vectoring Nozzle
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Airforce engineering university,Airforce engineering university,Airforce engineering university,Airforce engineering university

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V231.1

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    Abstract:

    Trustvectoring nozzle can visibly enhance the maneuverability of aircraft. The applications of mechanical vectoringnozzle are limited due to the complicated structure and poor reliability, while the pneumatic vectoringnozzle has a better performance. Series of pneumatic vectoringnozzle are developed in recent years. The development of pneumaticvectorcontrol technology is introduced briefly. The research progress on the aerodynamic performance and configuration optimization of dual throat nozzle is reviewed in detail. Problems in existing research are summarized and the future developments of dual throat nozzle are prospected.

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XIA Xuefeng, GAO Feng, HUANG Guibin, YANG Wenjia. Research Progress of the Dual-throat Thrust-vectoring Nozzle[J]. Advances in Aeronautical Science and Engineering,2017,8(3):249-255

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History
  • Received:January 19,2017
  • Revised:March 17,2017
  • Adopted:April 19,2017
  • Online: September 08,2017
  • Published: