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High-Resolution Skin-Friction Measurement Technique Based onOptical Flow Algorithm

Research Project

Project/Area Number 23656126
Research Category

Grant-in-Aid for Challenging Exploratory Research

Allocation TypeMulti-year Fund
Research Field Fluid engineering
Research InstitutionTohoku University

Principal Investigator

ASAI Keisuke  東北大学, 大学院・工学研究科, 教授 (40358669)

Co-Investigator(Kenkyū-buntansha) NUMATA Daiju  東北大学, 大学院・工学研究科, 助教 (20551534)
Project Period (FY) 2011 – 2012
Project Status Completed (Fiscal Year 2012)
Budget Amount *help
¥3,900,000 (Direct Cost: ¥3,000,000、Indirect Cost: ¥900,000)
Fiscal Year 2012: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2011: ¥2,990,000 (Direct Cost: ¥2,300,000、Indirect Cost: ¥690,000)
Keywords流体計測 / オプチカルフロー / せん断応力 / 流れの可視化 / 画像処理 / 蛍光油膜 / 可視化
Research Abstract

As a tool for visualizing two-dimensional skin-friction distribution on model surfaces, a new technique named “Global Luminescent Oil-Flow (GLOF)" technique has been developed. This method uses “optical flow" technique and extracts skin-friction vector field from time-series of oil-flow images. The accuracy and resolution of this technique were evaluated by applying to square cylinder and NACA-0012 airfoil testing. We found that GLOF allows us to measure skin friction distribution under the complex flow field including the reverse-flow region of a laminar separation bubble.

Report

(3 results)
  • 2012 Annual Research Report   Final Research Report ( PDF )
  • 2011 Research-status Report
  • Research Products

    (19 results)

All 2013 2012 2011

All Presentation (19 results)

  • [Presentation] Influenceof Turbulence Intensity on Aerodynamic Characteristics of an NACA 0012 at Low Reynolds Numbers2013

    • Author(s)
      Takaaki Tsuchiya, Daiju Numata, Tetsuya Suwa, Keisuke Asai
    • Organizer
      51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
    • Place of Presentation
      Grapevine, USA
    • Related Report
      2012 Final Research Report
  • [Presentation] Evaluation of free- stream turbulence intensity in the Mars Wind Tunnel under low Reynolds number conditions2013

    • Author(s)
      Daiju Numata, Takaaki Tsuchiya and Keisuke Asai
    • Organizer
      51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
    • Place of Presentation
      Grapevine, USA
    • Related Report
      2012 Final Research Report
  • [Presentation] Evaluation of free-stream turbulence intensity in the Mars Wind Tunnel under low Reynolds number conditions2013

    • Author(s)
      Daiju Numata
    • Organizer
      51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
    • Place of Presentation
      Grapevine, USA
    • Related Report
      2012 Annual Research Report
  • [Presentation] Influence of Turbulence Intensity on Aerodynamic Characteristics of an NACA 0012 at Low Reynolds Numbers2013

    • Author(s)
      Takaaki Tsuchiya
    • Organizer
      51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
    • Place of Presentation
      Grapevine, USA
    • Related Report
      2012 Annual Research Report
  • [Presentation] 低Re数翼の空力特性に対する乱流装置の効果2012

    • Author(s)
      中村勘太,依田大輔,沼田大樹,姜欣,近野敦,浅井圭介
    • Organizer
      日本航空宇宙学会北部支部2012年講演会ならびに第13回再使用型宇宙推進系シンポジウム
    • Place of Presentation
      室蘭工業大学,北海道
    • Year and Date
      2012-03-15
    • Related Report
      2012 Final Research Report
  • [Presentation] 火星大気風洞の主流乱れの制御と翼型特性への影響2012

    • Author(s)
      沼田大樹
    • Organizer
      平成24年度宇宙航行の力学シンポジウム
    • Place of Presentation
      相模原,日本
    • Related Report
      2012 Final Research Report
  • [Presentation] 低レイノルズ数におけるNACA0012翼型の空力特性に与える主流乱れ度の影響2012

    • Author(s)
      沼田大樹,土屋貴明,浅井圭介
    • Organizer
      第56回宇宙科学技術連合講演会
    • Place of Presentation
      別府,日本
    • Related Report
      2012 Final Research Report
  • [Presentation] 翼面上の2次元摩擦応力分布の光学的測定法2012

    • Author(s)
      中村勘太,依田大輔,沼田大樹,永井大樹,浅井圭介
    • Organizer
      第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012
    • Place of Presentation
      富山,日本
    • Related Report
      2012 Final Research Report
  • [Presentation] Compressibility Effect on Airfoil Aerodynamics at Low Reynolds Number2012

    • Author(s)
      Tetsuya Suwa, Kei Nose, Daiju Numata, Hiroki Nagai and Keisuke Asai
    • Organizer
      AIAA Fluid Dynamics and Co-located Conferences and Exhibit
    • Place of Presentation
      New Orleans,USA
    • Related Report
      2012 Final Research Report
  • [Presentation] 翼面上の2次元摩擦応力分布の光学的測定法2012

    • Author(s)
      中村勘太
    • Organizer
      第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012
    • Place of Presentation
      富山,日本
    • Related Report
      2012 Annual Research Report
  • [Presentation] 低レイノルズ数におけるNACA0012翼型の空力特性に与える主流乱れ度の影響2012

    • Author(s)
      沼田大樹
    • Organizer
      第56回 宇宙科学技術連合講演会
    • Place of Presentation
      別府,日本
    • Related Report
      2012 Annual Research Report
  • [Presentation] 火星大気風洞の主流乱れの制御と翼型特性への影響2012

    • Author(s)
      沼田大樹
    • Organizer
      平成24年度 宇宙航行の力学シンポジウム
    • Place of Presentation
      相模原,日本
    • Related Report
      2012 Annual Research Report
  • [Presentation] 低レイノルズ数領域において気体の圧縮性が翼性能に与える影響2012

    • Author(s)
      諏訪哲也
    • Organizer
      平成24年度 宇宙航行の力学シンポジウム
    • Place of Presentation
      相模原,日本
    • Related Report
      2012 Annual Research Report
  • [Presentation] Compressibility Effect on Airfoil Aerodynamics at Low Reynolds Number2012

    • Author(s)
      Suwa, T
    • Organizer
      AIAA Fluid Dynamics and Co-located Conferences and Exhibit
    • Place of Presentation
      New Orleans,USA
    • Related Report
      2012 Annual Research Report
  • [Presentation] 低Re数翼の空力特性に対する乱流装置の効果2012

    • Author(s)
      中村勘太,依田大輔,沼田大樹,姜 欣,近野敦,浅井圭介
    • Organizer
      日本航空宇宙学会北部支部2012年講演会ならびに第13回再使用型宇宙推進系シンポジウム
    • Place of Presentation
      室蘭工業大学,北海道
    • Related Report
      2011 Research-status Report
  • [Presentation] Evaluation of Aerodynamic Characteristics of a Triangular Airfoil at Low Reynolds Number and High-Subsonic Mach Number2011

    • Author(s)
      Suwa, T., Nose, K., Numata, D., Nagai, H., and Asai, K.
    • Organizer
      Eighth International Conference on Flow Dynamics (ICFD2011)
    • Place of Presentation
      仙台
    • Year and Date
      2011-11-10
    • Related Report
      2012 Final Research Report
  • [Presentation] 低レイノルズ数・高亜音速領域における三角翼型の空力特性の評価2011

    • Author(s)
      諏訪哲也,野瀬慶,沼田大樹,永井大樹,浅井圭介
    • Organizer
      第43回流体力学講演会
    • Place of Presentation
      東京
    • Year and Date
      2011-07-07
    • Related Report
      2012 Final Research Report
  • [Presentation] Evaluation of Aerodynamic Characteristics of a Triangular Airfoil at Low Reynolds Number and High-Subsonic Mach Number2011

    • Author(s)
      Suwa, T., Nose, K., Numata, D., Nagai, H., and Asai, K.
    • Organizer
      Eighth International Conference on Flow Dynamics (ICFD 2011)
    • Place of Presentation
      仙台国際センター,仙台
    • Related Report
      2011 Research-status Report
  • [Presentation] 低レイノルズ数・高亜音速領域における三角翼型の空力特性の評価2011

    • Author(s)
      諏訪哲也, 野瀬慶, 沼田大樹, 永井大樹, 浅井圭介
    • Organizer
      第43回流体力学講演会
    • Place of Presentation
      早稲田大学,東京
    • Related Report
      2011 Research-status Report

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Published: 2011-08-05   Modified: 2019-07-29  

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