• DocumentCode
    1594405
  • Title

    Model development for a dielectric barrier discharge plasma actuator for active flow control in Immersed bodies

  • Author

    Schneck, W.C. ; Winfrey, A.L.

  • Author_Institution
    Dept. of Mech. Eng. Blacksburg, Virginia Polytech. Inst. & State Univ., Blacksburg, VA, USA
  • fYear
    2013
  • Firstpage
    1
  • Lastpage
    1
  • Abstract
    Summary form only given. Immersed bodies such as struts, vanes, and instrumentation probes in gas turbine flow systems will, except at the lowest of flow velocities, shed separated wakes. These wakes can have both upstream and downstream effects on the surrounding flow. In most applications, surrounding components are designed to be in the presence of a quasi-steady or at least non-variant flow field. The presence of unsteady wakes has both aerodynamic and structural consequences. Active flow control of wake generation can therefore be very valuable.
  • Keywords
    aerodynamics; discharges (electric); electric actuators; flow control; plasma devices; plasma flow; plasma instability; wakes; active flow control; aerodynamics; dielectric barrier discharge plasma actuator; flow downstream effect; flow upstream effect; flow velocity; gas turbine flow system; immersed body; instrumentation probe; least non-variant flow field; quasisteady flow field; strut; unsteady wake; vane; wake generation; wake separation; Actuators; Computational modeling; Dielectrics; Electric fields; Plasmas; Power supplies; Surface treatment;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Plasma Science (ICOPS), 2013 Abstracts IEEE International Conference on
  • Conference_Location
    San Francisco, CA
  • ISSN
    0730-9244
  • Type

    conf

  • DOI
    10.1109/PLASMA.2013.6634912
  • Filename
    6634912