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Study on Flow Mechanism of Pseudo-Shock Waves in Scramjet Engine Isolators

Research Project

Project/Area Number 20560166
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Fluid engineering
Research InstitutionThe University of Kitakyushu

Principal Investigator

YOSHIAKI Miyazato  The University of Kitakyushu, 国際環境工学部, 教授 (30253537)

Project Period (FY) 2008 – 2010
Project Status Completed (Fiscal Year 2010)
Budget Amount *help
¥4,680,000 (Direct Cost: ¥3,600,000、Indirect Cost: ¥1,080,000)
Fiscal Year 2010: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2009: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2008: ¥2,600,000 (Direct Cost: ¥2,000,000、Indirect Cost: ¥600,000)
Keywords分離部 / ショックトレーン / 擬似衝撃波 / シュリーレン法 / 曲り管 / レインボーシュリーレン偏向法 / 境界層 / 通しピトー管 / カラーシュリーレン / 流れモデル / レインボーシュリーレン
Research Abstract

A normal shock wave in a constant area duct such as an isolator in a scram jet engine interacts with a wall boundary layer to form a pseudo-shock wave. Effects of the upstream boundary layer on a pseudo-shock wave are experimentally and theoretically clarified. Also, an optical system for measuring a complex shock containing supersonic flow quantitatively is presented. Further, compressible flow in curved ducts is experimentally studied.

Report

(4 results)
  • 2010 Annual Research Report   Final Research Report ( PDF )
  • 2009 Annual Research Report
  • 2008 Annual Research Report
  • Research Products

    (25 results)

All 2011 2010 2009 2008

All Journal Article (10 results) (of which Peer Reviewed: 10 results) Presentation (15 results)

  • [Journal Article] Measurements in Overexpanded Supersonic Jets by Rainbow Schlieren Deflectometry, 49th AIAA Aerospace Sciences Meeting2011

    • Author(s)
      Miyazato Y., Ishida, Y., Yamamoto H., Matsuo K.
    • Journal Title

      AIAA Paper No.2011-984,CD-ROM

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Journal Article] 曲り管内の圧縮流れに関する実験2010

    • Author(s)
      山本秀樹, 柳裕樹, 安信強, 宮里義昭, 松尾一泰
    • Journal Title

      可視化情報 30巻,増刊2号

      Pages: 183-184

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Journal Article] レインボーシュリーレン偏向法による適正膨張超音速噴流の計測2010

    • Author(s)
      宮里義昭, 入江将之, 山本秀樹, 松尾一泰
    • Journal Title

      日本機械学会論文集 76巻,768号

      Pages: 1129-1133

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Journal Article] Application of Rainbow Schlieren Deflectometry for Axisymmetric Supersonic Jets (Comparison of Experiments with Numerical Analysis)2010

    • Author(s)
      山本秀樹, 入江将之, 宮里義昭, 松尾一泰
    • Journal Title

      J. of Thermal Science Vol.19, No.3

      Pages: 218-221

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Journal Article] Quantitative Flow Visualization of Correctly Expanded Supersonic Jets by Rainbow Schlieren Deflectometry, 48th AIAA Aerospace Sciences Meeting2010

    • Author(s)
      宮里義昭, 入江将之, 山本秀樹, 松尾一泰
    • Journal Title

      AIAA Paper No.2010-1218,CD-ROM

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Journal Article] Application of Rainbow Schlieren Deflectometrt for Axisymmetric Supersonic Jets (Comparison of Experiments with Numerical Analysis)2010

    • Author(s)
      Yamamoto, H., Irie, M., Miyazato, Y., Matsuo, K
    • Journal Title

      Journal of Thermal Science

      Volume: Vol.19 Pages: 218-221

    • Related Report
      2010 Annual Research Report
    • Peer Reviewed
  • [Journal Article] 曲り管内の圧縮流れに関する実験2010

    • Author(s)
      山本秀樹, 柳裕樹, 安信強, 宮里義昭, 松尾一泰
    • Journal Title

      可視化情報

      Volume: 30 Pages: 183-184

    • Related Report
      2010 Annual Research Report
    • Peer Reviewed
  • [Journal Article] レインボーシュリーレン偏向法による適正膨張超音速噴流の計測2010

    • Author(s)
      宮里義昭, 入江将之, 山本秀樹, 松尾一泰
    • Journal Title

      日本機械学会論文集

      Volume: 76巻 Pages: 1129-1133

    • Related Report
      2010 Annual Research Report
    • Peer Reviewed
  • [Journal Article] Experimental and Theoretical Investigations of Normal Shock Wave/Turbulent Boundary-Layer Interactions at Law Mach Numbers in a Square Straight Duct, 47th AIAA Aerospace Sciences Meeting2009

    • Author(s)
      宮里義昭, 松尾一泰
    • Journal Title

      AIAA Paper No.2009-925,CD-ROM

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Journal Article] レインボーシュリーレン偏向法による軸対称超音速噴流の密度計測2009

    • Author(s)
      宮里義昭, 吉村文, 入江将之, 山本秀樹, 松尾一泰
    • Journal Title

      可視化情報 29巻,増刊2号

      Pages: 185-186

    • NAID

      10026050151

    • Related Report
      2010 Final Research Report
    • Peer Reviewed
  • [Presentation] Measurements in Overexpanded Supersonic Jets by Rainbow Schlieren Deflectometry2011

    • Author(s)
      Miyazato Y., Ishida Y., Yamamoto H., Matsuo K.
    • Organizer
      49th AIAA Aerospace Sciences Meeting, AIAA Paper, No. 2011-984
    • Place of Presentation
      Florida, USA(CD-ROM)
    • Related Report
      2010 Final Research Report
  • [Presentation] Measurements in Overexpanded Supersonic Jets by Rainbow Schlieren Deflectometry2011

    • Author(s)
      Miyazato, Y., Ishida, Y., Yamamoto, H., Matsuo, K.
    • Organizer
      49th AIAA Aerospace Sciences Meeting
    • Place of Presentation
      Florida, T SA
    • Related Report
      2010 Annual Research Report
  • [Presentation] 曲り管内の圧縮流れに関する実験2010

    • Author(s)
      山本秀樹, 柳裕樹, 安信強, 宮里義昭, 松尾一泰
    • Organizer
      可視化情報,30巻,増刊2号 pp.183-184
    • Place of Presentation
      名古屋
    • Related Report
      2010 Final Research Report
  • [Presentation] Quantitative Flow Visualization of Correctly Expanded Supersonic Jets by Rainbow Schlieren Deflectometry2010

    • Author(s)
      宮里義昭, 入江将之, 山本秀樹, 松尾一泰
    • Organizer
      48th AIAA Aerospace Sciences Meeting, AIAA Paper, No.2010-1218
    • Place of Presentation
      Florida, USA(CD-ROM)
    • Related Report
      2010 Final Research Report
  • [Presentation] Experimental and Theoretical Investigations of Normal Shock Wave/Turbulent Boundary-Layer Interactions at Law Mach Numbers in a Square Straight Duct2009

    • Author(s)
      宮里義昭, 松尾一泰
    • Organizer
      47th AIAA Aerospace Sciences Meeting, AIAA Paper, No.2009-925
    • Place of Presentation
      Florida, USA(CD-ROM)
    • Related Report
      2010 Final Research Report
  • [Presentation] レインボーシュリーレン偏向法による軸対称超音速噴流の密度計測2009

    • Author(s)
      宮里義昭, 吉村文, 入江将之, 山本秀樹, 松尾一泰
    • Organizer
      可視化情報,29巻,増刊2号 pp.185-186
    • Place of Presentation
      米沢
    • Related Report
      2010 Final Research Report
  • [Presentation] Application of Rainbow Schlieren Deflectometry for Axisymmetric Supersonic Jets (Comparison of Experiments with Numerical Analysis)2009

    • Author(s)
      山本秀樹, 入江将之, 宮里義昭, 松尾一泰
    • Organizer
      Proceedings of 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows
    • Place of Presentation
      Gyeongju, Korea
    • Related Report
      2010 Final Research Report
  • [Presentation] Application of Rainbow Schlieren Deflectometry for Axisymmetric Supersonic Jets (Experimental Investigations)2009

    • Author(s)
      宮里義昭, 山本秀樹, 吉村文, 尾一泰
    • Organizer
      Proceedings of 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Matsue
    • Place of Presentation
      Gyeongju, Korea
    • Related Report
      2010 Final Research Report
  • [Presentation] レインボーシュリーレン光学計測に関する基礎実験2009

    • Author(s)
      宮里義昭, 吉村文, 入江将之, 松尾一泰
    • Organizer
      平成20年度衝撃波シンポジウム講演論文集
    • Place of Presentation
      名古屋
    • Related Report
      2010 Final Research Report
  • [Presentation] 断面積一定の管内における低マッハ数の垂直衝撃波と乱流境界層の干渉2009

    • Author(s)
      宮里義昭, 笠田亮, 松尾一泰
    • Organizer
      日本機械学会流体工学部門講演論文集
    • Place of Presentation
      名古屋
    • Related Report
      2010 Final Research Report
  • [Presentation] 断面積一定の管内における低マッハ数の垂直衝撃波と乱流境界層の干渉2009

    • Author(s)
      宮里義昭, 笠田亮, 松尾一泰
    • Organizer
      日本機械学会流体工学部門講演会講演論文集
    • Place of Presentation
      名古屋大学
    • Related Report
      2009 Annual Research Report
  • [Presentation] Expenmental and Theoretical Investigations of Normal Shock Wave/Turbulent Boundary-Layer Interactions at Low Mach Numbers in a Square Straight Duct2009

    • Author(s)
      Miyazato, Y, Matuo, K, Kasada, R
    • Organizer
      47^<th> AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
    • Place of Presentation
      Florida, USA
    • Related Report
      2008 Annual Research Report
  • [Presentation] レインボーシュリーレン光学計測に関する基礎実験2009

    • Author(s)
      宮里義昭, 吉村文, 入江将之, 松尾一泰
    • Organizer
      平成20年度衝撃波シンポジウム
    • Place of Presentation
      名古屋大学
    • Related Report
      2008 Annual Research Report
  • [Presentation] Investigation of Weak Normal Shock Wave/Laminar Boundary Layer Interactions in Ducts2008

    • Author(s)
      Miyazato Y., Yaji, H., Matsuo K.
    • Organizer
      Proceedings of 12th Asian Congress of Fluid Mechanics
    • Place of Presentation
      Daejeon, Koria(CD-ROM)
    • Related Report
      2010 Final Research Report
  • [Presentation] Investigations of Weak Normal Shock Wave/Laminar Boundary Layer Interactions in Ducts2008

    • Author(s)
      Miyazato, Y, Yaji, H, Matsuo, K
    • Organizer
      12^<th> Asian Congress of Fluid Mechanics
    • Place of Presentation
      Daejeon, Koria.
    • Related Report
      2008 Annual Research Report

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Published: 2008-04-01   Modified: 2016-04-21  

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