Comparative study of co-flow and counter blowing DBD plasma actuators for separated flow over an airfoil

Satoshi Sekimoto, Kengo Asada, Masayuki Anyoji, Taku Nonomura, Kozo Fujii

研究成果: Contribution to conferencePaper

14 引用 (Scopus)

抜粋

A comparative study of co-flow and counter-blowing dielectric barrier discharge plasma actuator for separation control is conducted. These actuators are applied with normal mode and burst mode, where normal mode represents the actuation with continuous alternative current (AC) input and burst mode represents the actuation with the AC input switched on and off periodically. They are used for controlling the separated flow around NACA0015 airfoil at low Reynolds number Rec = 6.3 × 104. Pressure measurement and particle image velocimetry are conducted. In this study, four cases are conducted changing blowing direction, co-flow or counter-blowing, and actuation mode, normal or burst. Comparison among four cases shows that the dominant factor for suppressing separation with burst actuation is promoting transition, regardless of blowing direction. It also shows that the dominant factor of co-flow normal actuation is direct momentum addition. Counter-blowing normal actuation cannot suppress separation with any input voltage. Focusing on the minimum input voltage for suppressing separation, effectiveness for each attached case is compared and it is revealed that burst actuation more or less includes the effect of direct momentum addition.

元の言語英語
DOI
出版物ステータス出版済み - 2012
イベント50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Nashville, TN, 米国
継続期間: 1 9 20121 12 2012

その他

その他50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
米国
Nashville, TN
期間1/9/121/12/12

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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  • これを引用

    Sekimoto, S., Asada, K., Anyoji, M., Nonomura, T., & Fujii, K. (2012). Comparative study of co-flow and counter blowing DBD plasma actuators for separated flow over an airfoil. 論文発表場所 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, 米国. https://doi.org/10.2514/6.2012-1137