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2012 Fiscal Year Final Research Report

A study of plasma flow field around dielectric barrier discharge plasma actuator for high velocity flow condition

Research Project

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Project/Area Number 23860077
Research Category

Grant-in-Aid for Research Activity Start-up

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionHokkaido University (2012)
Japan Aerospace Exploration Agency (2011)

Principal Investigator

TAKAHASHI Yusuke  北海道大学, 大学院・工学研究院, 助教 (40611132)

Project Period (FY) 2011 – 2012
Keywordsプラズマ流 / 数値解析 / 熱化学的非平衡流
Research Abstract

Final goal of the present research is to develop a high-performance plasma actuator which is applicable for a condition of high-velocity flow. In the present study, to describe plasma flow behavior and potential drop by cathode sheath, numerical simulation models of plasma flow generated by dielectric barrier discharge plasma actuator and plasma near an electrode has been suggested and developed.

  • Research Products

    (1 results)

All 2012

All Journal Article (1 results)

  • [Journal Article] Improvement of Potential Drop Predictions for Plasma Wind Tunnels by Cathode Sheath2012

    • Author(s)
      Yusuke Takahashi, Hisashi Kihara,Ken-ichi Abe
    • Journal Title

      Journal of Thermophysics and Heat transfer

      Volume: Vol.26 Pages: 540-544

URL: 

Published: 2014-08-29  

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