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APPLICATION OF NON-LINEAR COMPACT SCHEMES TO COMPLEX TURBULENCE DIRECT NUMERICAL SIMULATIONS SUCH AS MULTI-PHASE FLOW

Research Project

Project/Area Number 13650169
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Fluid engineering
Research InstitutionHIROSHIMA UNIVERSITY (2002)
The University of Electro-Communications (2001)

Principal Investigator

MAEKAWA Hiroshi  GRADUATE SCHOOL OF ENGINEERING, PROFESSOR, 大学院・工学研究科, 教授 (90145459)

Project Period (FY) 2001 – 2002
Project Status Completed (Fiscal Year 2002)
Budget Amount *help
¥3,600,000 (Direct Cost: ¥3,600,000)
Fiscal Year 2002: ¥1,000,000 (Direct Cost: ¥1,000,000)
Fiscal Year 2001: ¥2,600,000 (Direct Cost: ¥2,600,000)
KeywordsComplex Turbulence / Compact Scheme / Multi-Phase Flow / Shock Wave / Convex Combined Scheme / Non-linear Filter / Acoustic Wave / Transition to Turbulence / DNS / WENO / 物理量不連続性 / 補間法 / 解像度 / 極超音速
Research Abstract

In this research project, application of non-linear compact schemes to simulations of complex turbulence with discontinuities, such as multi-phase flow turbulence, is studied. Compact schemes have a few advantages of high-resolution and minimum phase-error for turbulence simulations. However, application of symmetric compact schemes without any nonlinear treatment to the flow with physical discontinuities has hardly been successful due to the schemes dispersion error. On the other hand, ENO-type schemes have too large dissipation error to resolve propagating acoustic waves. In this project, three test problems have been investigated; (1) High Mach number blunt body flow receptivity to external acoustic waves, (2) Acoustic wave emission mechanism from supersonic shear layer, (3) Bubble collapse and microjet. Upwind compact schemes have an advantage to resolve the flow fields up to rather high-wavenumber and present a dissipation effect to damp numerical oscillation at only high-wavenumbers Advanced treatments of these schemes, such as convex combination of numerical flux, were proved to be successful to capture both large discontinuities and very small acoustic waves, For bubble distortion and breakdown simulations, a non-linear filter technique was employed.

Report

(3 results)
  • 2002 Annual Research Report   Final Research Report Summary
  • 2001 Annual Research Report
  • Research Products

    (58 results)

All Other

All Publications (58 results)

  • [Publications] D.Watanabe: "Transition of Supersonic Plane Jet due to Symmetric/Antisymmetric Unstable Modes"Journal of Turbulence (IOP). Vol.3. 1-17 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M.Yahyaoui: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows"Computational Fluid Dynamics Journal. Vol.11,No.2. 195-207 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M.Yahyaoui: "High-Level Noise Induced Bypass Transition in Compressible Plane Poisueille Flow"JSME International Journal. Vol.45,No.2. 408-418 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M.Yahyaoui: "Direct Numerical Simulations of Subsonic Plane Poiseuille Flows Undergoing Transition"JSME International Journal. Vol.44,No.1. 72-80 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H.Maekawa: "Study of Mach Wave Emission Mechanism in a Turbulent Jet at High Convective Mach Numbers Using DNS"Russia-Japan International Workshop on Actual Problems of Computational Mechanics. 招待講演. 32-33 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] K.Yamashita: "DNS of Hypersonic Boundary Layer Receptivity Using Compact Convex Combined Schemes"AIAA 10^<th> International Space Planes and Hypersonic Systems and Technologies Conference. No.1798. 1-11 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D.Watanabe: "Structures in a Supersonic Plane Jet due to Symmetric/Antisymmetric Unstable Modes at High Mach Number"Proc. of International Workshop on Prediction of Laminar-Turbulent Transition in Boundary Layers. NAL special Publication SP-48T. 39-42 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D.Watanabe: "Transition of Supersonic Plane Jet due to Symmetric/Antisymmetric Unstable Modes"Proc. of International Conference on Turbulent Shear Flow Phenomena. Vol.1. 419-424 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H.Maekawa: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows"Proc. of Japan-Russia International Workshop on Turbulence, Instabilities and Parallel Computing. (招待講演). 21-22 (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 渡邊大輔: "DNSによる超音速自由せん断流における音波放出機構の研究"航空宇宙数値シミュレーション技術シンポジウム講演論文集. NAL special Publication SP. 72-77 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 斉藤史徳: "不連続性を捕らえる高次風上コンパクトスキームを用いたCFD"日本流体力学会 年会2002講演論文集. 332-333 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 竹原洋三: "圧縮性乱流DNSを使ったLESモデルの評価と比較"日本流体力学会 年会2002講演論文集. 396-397 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 青木崇志: "超音速混合層の安定性と渦構造に及ぼすマッハ数の影響"日本機械学会関東支部第8期総会講演会. No.1011. (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 奥村学: "空間発展DNSによる水素、空気拡散火炎の火炎構造"日本機械学会関東支部第8期総会講演会. No.515. (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 相沢寛朗: "DNSによる水素・空気噴流火炎の燃焼音に関する研究"第39回燃焼シンポジウム. A214. (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 尾崎幸玄: "矩形断面を持つ曲がりダクト内の圧縮性粘性流れの解析"第16回数値流体力学シンポジウム. E14-4. (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H.Maekawa: "Convex Combined Compact Schemes for Turbulence Simulations with Discontinuities"生産NSTシンポジウム講演論文集. (2001)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] X.Deng: "Applications of fifth-order weighted compact nonlinear schemes to Euler and Navier-Stokes equations"Proc. of 4th Asian CFD Conference. 396-397 (2000)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] 前川 博: "対話とシミュレーションムービーでまなぶ 流体力学"共立出版. 147 (2002)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D. Watanabe: "Transition of Supersonic Plan Jet due to Symmetric / Antisymmetric Unstable Modes"Journal of Turbulence (IOP). 3. 1-7 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M. Yahyaoui: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows"Computational Fluid Dynamics Journal. 11, No.2. 195-207 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M. Yahyaoui: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows"Computational Fluid Dynamics Journal. 11, No.2. 195-207 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M. Yahyaoui: "High-Level Noise Induced Bypass Transition in Compressible Plane Poiseuille Flow"JSME International Journal. 45, No.2. 408-418 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M. Yahyaoui: "Direct Numerical Simulations of Subsonic Plane Poiseuille Flows Undergoing Transition"JSME International Journal. 44, No.1. 72-80 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H. Maekawa: "Study of Mach Wave Emission Mechanism in a Turbulent Jet at High Convective Mach Numbers Using DNS, (invited)"Proc. Of Russia-Japan International Workshop on Actual Problems of Computational Mechanics. 32-33 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] K. Yamashita: "DNS of Hypersonic Boundary Layer Receptivity Using Compact Convex Combined Schemes"AIAA 10^<th> International Space Planes and Hypersonic Systems and Technologies Conference. 1798. 1-11 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D. Watanabe: "Structures in a Supersonic Plane Jet due to Symmetric / Antisymmetric Unstable Modes at High Mach Number, (invited)"Proc. Of International Workshop on Prediction of Laminar-Turbulent Transition in Boundary Layers, NAL special Publication. SP-48T. 39-42 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D. Watanabe: "Transition of Supersonic Plane Jet due to Symmetric / Antisymmetric Unstable Modes"Proc. Of International Conference on Turbulent Shear Flow Phenomena. 1. 419-424 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H. Maekawa: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows, (invited)"Proc. Of Japan-Russia International Workshop on Turbulence, Instabilities and Parallel Computing. 21-22 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D. Watanabe: "A study of sound wave emission mechanism in supersonic free shear flows using DNS, (in Japanese)"NAL Aerospace and Aeronautics Simulation Symposium 2002. (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] F. Saito: "High-order Upwind Compact Schemes for Flow Field with discontinuities. (in Japanese)"Fluid Mechanics Society Annual meeting 2002.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] T. Aoki: "Effect of Mach number on stability and vortex structure of a supersonic mixing layer,(in Japanese)"JSME Kanto-Branch 8^<th> symposium and meeting. (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] M. Okumura: "Spatially developing DNS of H2-Air diffusion frame structures, (in Japanese)"JSME Kanto-Branch 8^<th> symposium and meeting. (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H. Aizawa: "Direct Numerical Simulation of Combustion Noise caused by Hydrogen / Air Jet Frames, (in Japanese)"39^<th> Combustion Symposium. (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] K. Ozaki: "Compressible and viscous flow in the curved duct with a squared section, (in Japanese)"16^<th> CFD Symposium. E14-4. (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H. Maekawa: "Convex Combined Compact Schemes for Turbulence Simulations with Discontinuities"Proc. Of NST Symposium. (2001)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] X. Deng: "Applications of fifth-order weighted compact nonlinear schemes to Euler and Navier-Stokes equations"Proc. Of 4th Asian CFD Conference. (2000)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] H. Maekawa: "Fluid Mechanics, (in Japanese)"Kyotitsu-Publication. 1-148 (2002)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2002 Final Research Report Summary
  • [Publications] D.Watanabe: "Transition of Supersonic Plane Jet due to Symmetric/Antisymmetric Unstable Modes"Journal of Turbulence(IOP). Vol.3. 1-17 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] M.Yahyaoui: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows"Computational Fluid Dynamics Journal. 11・2. 195-207 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] M.Yahyaoui: "High-Level Noise Induced Bypass Transition in Compressible Plane Poisueille Flow"JSME International Journal. 45・2. 408-418 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] M.Yahyaoui: "Direct Numerical Simulations of Subsonic Plane Poiseuille Flows Undergoing Transition"JSME International Journal. 44・1. 72-80 (2001)

    • Related Report
      2002 Annual Research Report
  • [Publications] H.Maekawa: "Study of Mach Wave Emission Mechanism in a Turbulent Jet at High Convective Mach Numbers Using DNS"Russia-Japan International Workshop on Actual Problems of Computational Mechanics. 招待講演. 32-33 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] K.Yamashita: "DNS of Hypersonic Boundary Layer Receptivity Using Compact Convex Combined Schemes"AIAA 10^<th> International Space Planes and Hypersonic Systems and Techonologies Conference. No.1798. 1-11 (2001)

    • Related Report
      2002 Annual Research Report
  • [Publications] D.Watanabe: "Structures in a Supersonic Plane Jet due to Symmetric/Antisymmetric Unstable Modes at High Mach Numbers"Proc. of International Workshop on Prediction of Laminar-Turbulent Transition in Boundary Layers. NAL Special Pub.SP-48T. 39-42 (2001)

    • Related Report
      2002 Annual Research Report
  • [Publications] D.Watanabe: "Transition of Supersonic Plane Jet due to Symmetric/Antisymmetric Unstable Modes"Proc. of International Conference on Turbulent Shear Flow Phenomena. Vol.1. 419-424 (2001)

    • Related Report
      2002 Annual Research Report
  • [Publications] M.Yahyaoui: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bouded Flows"Proc. of Japan-Russia International Workshop on Turbulence, Instabilities and Parallel Computing. 招待講演. 21-22 (2001)

    • Related Report
      2002 Annual Research Report
  • [Publications] 前川 博: "対話とシミュレーションムービーでまなぶ流体力学"共立出版. 147 (2002)

    • Related Report
      2002 Annual Research Report
  • [Publications] 山下 建志, 前川 博: "非線形コンパクトスキームの改良と圧縮性DNSへの応用"第14回数値流体力学シンポジウム講演論文集. ISSN1344-4602. E03-4 (2000)

    • Related Report
      2001 Annual Research Report
  • [Publications] H.Maekawa, K.Yamashita, X.Deng: "Convex Combined Compact Schemes for Turbulence Simulations with Discontinuities"Proc. of 16^<th> Numerical Simulation ofTurbulence Symposium. 42-47 (2001)

    • Related Report
      2001 Annual Research Report
  • [Publications] K.Yamashia, H.Maekawa: "Direct Numerical Simulations of Hypersonic Boundary Layer Receptivity Using Compact Convex Combined Schemes"AIAA 10^<th> International Space Planes and Hypersonic Systems and Technology Confereiice. AIAA2001-1798. (2001)

    • Related Report
      2001 Annual Research Report
  • [Publications] A.M.Yahyaoui, H.Maekawa: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows"Computational Fluid Dynamics Journal. Vol.11, No.1. (2002)

    • Related Report
      2001 Annual Research Report
  • [Publications] A.M.Yahyaoui, H.Maekawa: "High Level Noise-Induced Bypass Transition in Compressible Plane Poiseeille Flow"JSME International Journal, Series B. Vol.45,No.2. (2002)

    • Related Report
      2001 Annual Research Report
  • [Publications] 相澤 寛朗, 前川 博: "DNSによる水素/空気噴流火炎の燃焼音に関する研究"第39回燃焼シンポジウム講演論文集. 169-170 (2001)

    • Related Report
      2001 Annual Research Report
  • [Publications] D.Watanabe, H.Maekawa: "Transition of Supersonic Plane Jet Due to Symmetric/Antisymmetric Unstable Modes"Proc. of Turbulence and Shear Flow-Phenomena. Vol.1. 419-424 (2001)

    • Related Report
      2001 Annual Research Report
  • [Publications] H.Maekawa. A.M.Yahyaoui: "Simulations of Bypass Transition for Spatially Evolving Disturbances in Compressible Wall-Bounded Flows(招待講演)"Proc. of Japan-Russia International Workshop on Turbulence, Instability and Parallel Computing. 24-25 (2001)

    • Related Report
      2001 Annual Research Report
  • [Publications] 青木 崇志, 渡邊 大輔, 前川 博: "超音速混合層の安定性と渦構造に及ぼすマッハ数の影響"日本機械学会関東支部第8期総会講演会講演論文集. (2002)

    • Related Report
      2001 Annual Research Report
  • [Publications] 奥村 学, 前川 博: "空間発展DNSによる水素、空気拡散火炎の火炎構造"日本機械学会関東支部第8期総会講演会講演論文集. (2002)

    • Related Report
      2001 Annual Research Report

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Published: 2001-04-01   Modified: 2016-04-21  

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