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Analysis of origin of Attached-Eddy in a boundary layer using significant slow transition

Research Project

Project/Area Number 17K06147
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeMulti-year Fund
Section一般
Research Field Fluid engineering
Research InstitutionThe University of Electro-Communications

Principal Investigator

Maekawa Hiroshi  電気通信大学, 大学院情報理工学研究科, 特命教授 (90145459)

Co-Investigator(Kenkyū-buntansha) 渡邊 大輔  富山大学, 学術研究部工学系, 講師 (70363033)
井上 洋平  電気通信大学, 大学院情報理工学研究科, 准教授 (40397625)
Project Period (FY) 2017-04-01 – 2023-03-31
Project Status Completed (Fiscal Year 2022)
Budget Amount *help
¥4,810,000 (Direct Cost: ¥3,700,000、Indirect Cost: ¥1,110,000)
Fiscal Year 2019: ¥260,000 (Direct Cost: ¥200,000、Indirect Cost: ¥60,000)
Fiscal Year 2018: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2017: ¥3,510,000 (Direct Cost: ¥2,700,000、Indirect Cost: ¥810,000)
Keywords圧縮性境界層 / 乱流遷移 / 乱流と音響場 / 国際研究集会 / 射影幾何学 / 楕円曲線 / バイパス遷移 / 超音速境界層 / マッハ数 / ワークショップ / 空力音響 / 乱流境界層 / Eddy構造 / 国際ワークショップ / 乱流 / 遷移 / 乱流Eddy / バイパス
Outline of Final Research Achievements

This study describes a self-sustained structure created from the rapid growth of unsteady finite-amplitude perturbations in a supersonic boundary layer. The localized incipient structure is identified as a long-lived structure with a pair of quasi-streamwise vortices with vorticity of alternate sign at a saddle point in the state space. The time averaged trajectories of the cross-flow energy in the state space indicate the geometric structure consisting of the stable and unstable manifolds around the saddle point. The long-lived structure creates the site of subharmonic and fundamental sinuous instabilities evolving into a turbulent spot with the pre-nucleation event of the spot. Temporal variations in the cross-flow energy on the unstable manifold clearly indicate the alternation of bursting and pre-nucleation phases. The escape process along the unstable manifold from the saddle point is characterized by the Weierstrass elliptic function.

Academic Significance and Societal Importance of the Research Achievements

研究成果の学術的意義は乱流遷移がWeierstrassの楕円関数によって特徴づけられることを明らかにしたことである.乱流遷移を代数幾何学で理解するプロセスを示した.楕円曲線と数論幾何学とは関係があり,乱流現象は整数論と繋がりがあることを研究成果は示唆している.社会的意義は,乱流遷移した乱流境界層が発達する物体からの音響場の発生は実社会への応用においていたるところに見られ,渦運動からの音響場が支配的になる新幹線の高速化における環境適合性の向上には欠かせない技術の進展や,遷移予測が各段に向上することを可能にしたことによって低燃費の航空機開発に寄与することである.

Report

(7 results)
  • 2022 Annual Research Report   Final Research Report ( PDF )
  • 2021 Research-status Report
  • 2020 Research-status Report
  • 2019 Research-status Report
  • 2018 Research-status Report
  • 2017 Research-status Report
  • Research Products

    (34 results)

All 2023 2021 2020 2019 2018 2017

All Journal Article (15 results) (of which Int'l Joint Research: 1 results,  Peer Reviewed: 15 results,  Open Access: 5 results) Presentation (18 results) Funded Workshop (1 results)

  • [Journal Article] Sound radiation by a vortex pair moving near a rectangular cylinder.2023

    • Author(s)
      鹿沼 剛,井上 洋平,前川 博
    • Journal Title

      Transactions of the JSME (in Japanese)

      Volume: 89 Issue: 917 Pages: 22-00223-22-00223

    • DOI

      10.1299/transjsme.22-00223

    • ISSN
      2187-9761
    • Related Report
      2022 Annual Research Report
    • Peer Reviewed
  • [Journal Article] Sound radiated from low Mach number turbulent boundary layer flows(Turbulent boundary layer on a smooth plate and over a small forward facing step)2021

    • Author(s)
      Shiko Moriyama, Yohei Inoue, Hiroshi Maekawa
    • Journal Title

      Journal of Fluid Science and Technology

      Volume: 16 Issue: 2 Pages: JFST0010-JFST0010

    • DOI

      10.1299/jfst.2021jfst0010

    • NAID

      130007966481

    • ISSN
      1880-5558
    • Related Report
      2020 Research-status Report
    • Peer Reviewed / Open Access
  • [Journal Article] 境界層中に設置された平板に作用する流体力2019

    • Author(s)
      井上洋平, 穂積尚門, 前川博
    • Journal Title

      ながれ

      Volume: 38 Pages: 348-356

    • NAID

      40022087357

    • Related Report
      2019 Research-status Report
    • Peer Reviewed / Open Access
  • [Journal Article] Study of the Interaction between Vortex and a Squire Cylinder with a part of Structure made by Flexible Material2019

    • Author(s)
      Hiroharu Matsubara, Wataru Nakayama, Yohei Inoue, Hiroshi Maekawa
    • Journal Title

      2019 AIAA Aviation Forum

      Volume: 1 Pages: 1-20

    • DOI

      10.2514/6.2019-3674

    • Related Report
      2019 Research-status Report
    • Peer Reviewed / Open Access
  • [Journal Article] Mach wave suppression by a pair of subsonic helical modes in a2019

    • Author(s)
      Daisuke Watanabe & Hiroshi Maekawa
    • Journal Title

      the 25th AIAA/CEAS Aeroacoustics Conference

      Volume: 1 Pages: 1-8

    • DOI

      10.2514/6.2019-2754

    • Related Report
      2019 Research-status Report
    • Peer Reviewed
  • [Journal Article] Sound Radiated from Low Mach Number Turbulent Boundary- layer Flows (Turbulent Boundary Layer On a Smooth Plate and Over a Forward Facing Step)2019

    • Author(s)
      Shikou Moriyama, Yohei Inoue, Hiroshi Maekawa
    • Journal Title

      Proc. 16th International Conference of Fluid Dynamics

      Volume: 1 Pages: 1-2

    • Related Report
      2019 Research-status Report
    • Peer Reviewed
  • [Journal Article] Numerical Investigation of Compressible Cross Jet with Temperature Difference2019

    • Author(s)
      Yohei Inoue,Takahiro Shimokawa , Hiroshi Maekawa
    • Journal Title

      Proc. 2nd Pacific Rim Thermal Engineering Conference

      Volume: 1 Pages: 1-5

    • Related Report
      2019 Research-status Report
    • Peer Reviewed
  • [Journal Article] Aeroacoustic Noise Generated by Air Flowing through a Slit in an HVAC System2019

    • Author(s)
      Tsuyoshi Kanuma, Yohei Inoue, Hiroshi Maekawa
    • Journal Title

      Proc. World Congress and Exhibition

      Volume: HX/0062 Pages: 1-8

    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Journal Article] Effects of Free Stream Disturbance on the Development of the Compressible Flow around a Square Cylinder at Subsonic Mach Numbers2018

    • Author(s)
      Yohei Inoue, Tsuyoshi Kanuma, Yuma Tasai, Hiroshi Maekawa
    • Journal Title

      Proc. 2018 AIAA Aviation Forum

      Volume: AA/54 Pages: 1-15

    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Journal Article] Effect of Upstream Disturbance on the Develop- ment of a Wall-Bounded Plane Jet at Subsonic Mach Numbers with Separated Flow2018

    • Author(s)
      Tsuyoshi Kanuma, Keisuke Kuramata, Yohei Inoue, Hiroshi Maekawa
    • Journal Title

      Proc. 2018 AIAA Aviation Forum

      Volume: FD/36 Pages: 1-15

    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Journal Article] Interaction between Flexible Structure and Compressible Flow2018

    • Author(s)
      Hiroharu Matsubara, Yohei Inoue, and Hiroshi Maekawa
    • Journal Title

      Proceedings of Ameical Physical Society Meeting

      Volume: G60 Pages: 348-348

    • Related Report
      2017 Research-status Report
    • Peer Reviewed / Open Access
  • [Journal Article] Transition of a compressible square cylinder wake structures subjected to free-stream disturbance2018

    • Author(s)
      Yuma TASAI, Yohei INOUE, Tsuyoshi KANUMA, Hiroshi MAEKAWA
    • Journal Title

      Proceedings of Ameical Physical Society Meeting

      Volume: L60 Pages: 340-340

    • Related Report
      2017 Research-status Report
    • Peer Reviewed
  • [Journal Article] Effects of Free Stream Disturbance on the Development of the Compressible Flow around a Square Cylinder at Subsonic Mach Numbers2018

    • Author(s)
      Yohei Inoue, Tsuyoshi Kanuma, Yuma Tasai, Hiroshi Maekawa
    • Journal Title

      Proceedings of AIAA Aviation Forum

      Volume: AA Pages: 1-15

    • Related Report
      2017 Research-status Report
    • Peer Reviewed
  • [Journal Article] Effects of Upstream Disturbance on the Develop- ment of a Wall-Bounded Plane Jet at Subsonic Mach Numbers with Separated Flow2018

    • Author(s)
      Tsuyoshi Kanuma, Keisuke Kuramata, Yohei Inoue, Hiroshi Maekawa
    • Journal Title

      Proceedings of AIAA Aviation Forum

      Volume: FD Pages: 1-11

    • Related Report
      2017 Research-status Report
    • Peer Reviewed
  • [Journal Article] Investigation and Control of Transition to Turbulence2017

    • Author(s)
      Editor Hiroshi Maekawa, Yohei Inoue, and Masaharu Mtsubara
    • Journal Title

      Proceedings of 61st Workshop on Investigation and Control of Transition to Turbulence

      Volume: 1 Pages: 1-18

    • Related Report
      2017 Research-status Report
    • Peer Reviewed / Open Access / Int'l Joint Research
  • [Presentation] 超音速ジェットの拡散に及ぼす撹乱速度成分の影響2020

    • Author(s)
      渡辺 大輔
    • Organizer
      宇宙航空研究開発機構特別資料JAXA-SP-19-007
    • Related Report
      2019 Research-status Report
  • [Presentation] 平板乱流境界層中に存在する微小ステップの高さが音響場に与える影響2019

    • Author(s)
      森山 史孝
    • Organizer
      第33回数値流体力学シンポジウム
    • Related Report
      2019 Research-status Report
  • [Presentation] 超音速ジェットの拡散に及ぼす縦渦の不安定性の影響2019

    • Author(s)
      渡辺 大輔
    • Organizer
      日本機械学会 2019年度年次大会
    • Related Report
      2019 Research-status Report
  • [Presentation] 圧縮性ジェットにおけるヘリカルモードペアの増幅に対するマッハ数の影響2019

    • Author(s)
      渡辺大輔
    • Organizer
      日本流体力学会 年会2019
    • Related Report
      2019 Research-status Report
  • [Presentation] 超音速ジェットから放射されるマッハ波に及ぼす流入撹乱成分の影響2019

    • Author(s)
      渡辺大輔
    • Organizer
      日本機械学会 第96期 流体工学部門 講演会
    • Related Report
      2019 Research-status Report
  • [Presentation] 超音速ジェットにおけるヘリカルモードの受容性に対する速度成分の影響2019

    • Author(s)
      渡辺 大輔
    • Organizer
      日本機械学会 北陸信越支部 第56期総会・講演会
    • Related Report
      2018 Research-status Report
  • [Presentation] 平行平板間噴流における上流撹乱の影響2018

    • Author(s)
      井上 洋平 鹿沼 剛 前川 博
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 低亜音速境界層における乱流遷移渦構造から発生する空力音の数値計算2018

    • Author(s)
      森山 史孝 井上 洋平 前川 博
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 超音速ジェットにおけるヘリカルモードペアを用いたマッハ波抑制のせん断層厚さの影響2018

    • Author(s)
      渡辺 大輔 石崎 匡則
    • Organizer
      第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 超音速平面ジェットにおけるノズルクラスタ化のマッハ波放射への影響2018

    • Author(s)
      渡辺 大輔 原田 天晴
    • Organizer
      日本機械学会 2018年度年次大会
    • Related Report
      2018 Research-status Report
  • [Presentation] 低い位相速度を持つヘリカルモードペアを用いた超音速ジェットのマッハ波抑制2018

    • Author(s)
      渡辺大輔、前川 博
    • Organizer
      日本機械学会 第96期 流体工学部門 講演会
    • Related Report
      2018 Research-status Report
  • [Presentation] 超音速境界層における長波長の主流乱れの遷移に及ぼす影響2018

    • Author(s)
      渡辺大輔、前川 博
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 超音速ジェットにおける非対称なヘリカルモード組合せの遷移構造への影響2017

    • Author(s)
      渡辺 大輔、広上 渓介、前川 博
    • Organizer
      日本機械学会 2017年度年次大会
    • Related Report
      2017 Research-status Report
  • [Presentation] 超音速円形ジェットの安定性に及ぼす速度分布の影響2017

    • Author(s)
      渡辺 大輔、前川 博
    • Organizer
      日本流体力学会 年会2017
    • Related Report
      2017 Research-status Report
  • [Presentation] 超音速co-flowジェットの遷移に対する流入撹乱の影響2017

    • Author(s)
      大和 優太、渡辺 大輔
    • Organizer
      第31回数値流体力学シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 圧縮性流れにおける様々な固体壁境界条件2017

    • Author(s)
      松原弘明,中山渉,井上洋平,前川博
    • Organizer
      第31回数値流体力学シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 鈍体後流構造へのジェットによる変調と流体抗力の関係2017

    • Author(s)
      井上洋平,前川博
    • Organizer
      第31回数値流体力学シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] 鈍体に設置された噴流による後流構造の変化2017

    • Author(s)
      井上洋平,前川博
    • Organizer
      日本流体力学会 年会2017
    • Related Report
      2017 Research-status Report
  • [Funded Workshop] Workshop on Investigation and Control of Transition to Turbulence2017

    • Related Report
      2017 Research-status Report

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Published: 2017-04-28   Modified: 2024-01-30  

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