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2010 Fiscal Year Final Research Report

Study of application and density measurements by focusing schlieren method in high speed flows

Research Project

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Project/Area Number 21760144
Research Category

Grant-in-Aid for Young Scientists (B)

Allocation TypeSingle-year Grants
Research Field Fluid engineering
Research Institution防衛大学校

Principal Investigator

KASHITANI Masashi  防衛大学校, システム工学群, 准教授 (80535279)

Project Period (FY) 2009 – 2010
Keywords流体計測 / 圧縮性流れ / シュリーレン法 / 三次元流れ / 衝撃波管 / 超音速複葉翼
Research Abstract

A large-field and a high-brightness focusing schlieren system was developed to visualize three-dimensional density gradients in flow fields. However, a quantitative experiment seems to be still few, and the accumulation of further data is necessary to verify the quantitative measurement technique. In the present study, a diaphragmless shock tube that is expected good stability and efficiency is used to produce basic flows. We discussed the characteristics of the quantitative parameter of the focusing schlieren system. The results are as follows, the density distributions across the incident shock wave almost correspond to the simple theory in the present study. And flow visualizations around the supersonic biplane airfoil were performed in the transonic shock tube flow by the focusing schlieren system.

  • Research Products

    (12 results)

All 2011 2010 2009

All Journal Article (5 results) (of which Peer Reviewed: 5 results) Presentation (7 results)

  • [Journal Article] 点回折干渉計による衝撃波管翼型流れの試験気体の影響に関する研究2011

    • Author(s)
      樫谷賢士, 山口裕, 沖元海
    • Journal Title

      日本航空宇宙学会論文集 59

      Pages: 34-41

    • Peer Reviewed
  • [Journal Article] Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method2011

    • Author(s)
      M.Kashitani, Y.Yamaguchi, H.Kitano
    • Journal Title

      AIAA Paper

      Pages: 2011-0983

    • Peer Reviewed
  • [Journal Article] フォーカシングシュリーレン画像による密度計測に関する基礎実験2010

    • Author(s)
      樫谷賢士, 山口裕, 北野秀樹
    • Journal Title

      可視化情報学会誌 Vol.30, Suppl.No.2

      Pages: 115-116

    • Peer Reviewed
  • [Journal Article] Visualizations around the 3-D Diamond Model with Trip Strips in Transonic Shock Tube Flows by Focusing Schlieren Method2010

    • Author(s)
      M.Kashitani, Y.Yamaguchi, G.Oki
    • Journal Title

      Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows No.5C-1

    • Peer Reviewed
  • [Journal Article] Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Testing2010

    • Author(s)
      M.Kashitani
    • Journal Title

      Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows No.4C-3

    • Peer Reviewed
  • [Presentation] Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method2011

    • Author(s)
      M.Kashitani, Y.Yamaguchi, H.Kitano
    • Organizer
      49th AIAA Aerospace Sciences Meeting
    • Place of Presentation
      Orlando
    • Year and Date
      2011-01-05
  • [Presentation] 高亜音速衝撃波管翼型流れの可視化2010

    • Author(s)
      山口裕, 沖元海, 宮崎大, 樫谷賢士, 江刺悟
    • Organizer
      第48回飛行機シンポジウム
    • Place of Presentation
      静岡
    • Year and Date
      2010-12-02
  • [Presentation] フォーカシングシュリーレン画像による密度計測に関する基礎実験2010

    • Author(s)
      樫谷賢士, 山口裕, 北野秀樹
    • Organizer
      可視化情報学会全国講演会
    • Place of Presentation
      鹿児島
    • Year and Date
      2010-10-07
  • [Presentation] 衝撃波管を用いた超音速複葉翼型流れに関する基礎研究2010

    • Author(s)
      樫谷賢士, 山口裕, 沖元海, 江刺悟, 楠瀬一洋
    • Organizer
      日本航空宇宙学会第41期年会講演会
    • Place of Presentation
      東京
    • Year and Date
      2010-04-16
  • [Presentation] OpenFOAMを用いた3次元模型周りの流れ場の診断2010

    • Author(s)
      江刺悟, 山口裕, 樫谷賢士, 沖元海
    • Organizer
      平成21年度衝撃波シンポジウム
    • Place of Presentation
      埼玉
    • Year and Date
      2010-03-17
  • [Presentation] Visualizations around the 3-D Diamond Model with Trip Strips in Transonic Shock Tube Flows by Focusing Schlieren Method2009

    • Author(s)
      M.Kashitani, Y.Yamaguchi, G.Oki
    • Organizer
      9th ISAIF
    • Place of Presentation
      Gyeongju
    • Year and Date
      2009-09-11
  • [Presentation] Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Testing2009

    • Author(s)
      M.Kashitani
    • Organizer
      9th ISAIF
    • Place of Presentation
      Gyeongju
    • Year and Date
      2009-09-11

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Published: 2012-02-13   Modified: 2016-04-21  

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