• DocumentCode
    2859740
  • Title

    Characteristics of PZT-driven dual synthetic jets actuator and numerical simulations of thrust vectoring

  • Author

    Luo, Zhen-bing ; Wang, Lin ; Wang, Deng-pan ; Xia, Zhi-xun

  • Author_Institution
    Coll. of Aerosp. & Mater. Eng., Nat. Univ. of Defense Technol., Changsha, China
  • fYear
    2010
  • fDate
    10-13 Dec. 2010
  • Firstpage
    254
  • Lastpage
    258
  • Abstract
    The characteristics of the novel dual synthetic jets actuator are summarized in this paper. The dual synthetic jets actuator not only resolves the problems of pressure loading and energy inefficiency of the traditional synthetic jet actuators, but also has unique thrust-vectoring characteristic itself by adjusting area ratio of the two exits or volume ratio of the two cavities of the dual synthetic jets actuator. A primary jet vectoring using the dual synthetic jets actuator is numerically simulated, and the results show a single dual synthetic jets actuator can play both “push” and “pull” functions of thrust-vectoring the primary jet, and its efficiency is higher than that of the traditional synthetic jet actuator (SJA), what´s more, the efficiency of its “push” functions is higher than that of “pull” functions.
  • Keywords
    actuators; jets; numerical analysis; PZT-driven actuator; actuator pull function; actuator push function; dual synthetic jets actuator; numerical simulation; thrust vectoring characteristic; Actuators; Aerospace engineering; Cavity resonators; Fluids; Loading; Physics; Dual synthetic jets actuator (DSJA); PZT-vibrator; characteristics; thrust vectoring;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Piezoelectricity, Acoustic Waves and Device Applications (SPAWDA), 2010 Symposium on
  • Conference_Location
    Xiamen
  • Print_ISBN
    978-1-4244-9822-2
  • Electronic_ISBN
    978-1-4244-9821-5
  • Type

    conf

  • DOI
    10.1109/SPAWDA.2010.5744315
  • Filename
    5744315