• Search Research Projects
  • Search Researchers
  • How to Use
  1. Back to previous page

Modeling for multi-component flows and combustion dynamics under supercritical pressure environments

Research Project

Project/Area Number 17K06939
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeMulti-year Fund
Section一般
Research Field Aerospace engineering
Research InstitutionHokkaido University

Principal Investigator

Terashima Hiroshi  北海道大学, 工学研究院, 准教授 (20415235)

Project Period (FY) 2017-04-01 – 2020-03-31
Project Status Completed (Fiscal Year 2019)
Budget Amount *help
¥4,550,000 (Direct Cost: ¥3,500,000、Indirect Cost: ¥1,050,000)
Fiscal Year 2019: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2018: ¥1,690,000 (Direct Cost: ¥1,300,000、Indirect Cost: ¥390,000)
Fiscal Year 2017: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
Keywords超臨界流体 / 燃焼 / 非理想性 / 数値シミュレーション / 非理想熱輸送物性 / 数値流体力学 / 火炎モデル / 非理想流体 / 超臨界圧流体 / 界面相変化
Outline of Final Research Achievements

This study has developed a simulation method for combustion and multi-component flow dynamics under supercritical pressures. The method introduced the non-ideal thermodynamic and transport property models to consider peculiar behaviors that appear in supercritical pressures. All the models were fully validated in comparison with experimental or reference data. The flame propagation problems under supercritical pressures demonstrated that the non-ideal effects in the diffusion coefficient are the most influential for the prediction of laminar flame speeds. Regarding thinner flame in higher-pressure conditions, we have developed a new flame model, with which the flame propagation behavior under elevated pressure conditions was successfully captured even on coarser grids. Besides, we constructed a non-ideal fluid library, with which the non-ideal thermodynamic and transport properties are easily obtained in arbitrary simulation programs.

Academic Significance and Societal Importance of the Research Achievements

現在,急速な温暖化をはじめとして地球環境問題の改善が喫緊の課題である.燃焼機器の熱効率向上を目的に,現在考慮されていないような超高圧環境下での燃焼技術が今後求められる可能性がある.本研究で開発した超臨界圧流体および燃焼シミュレーション技術は,従来のシミュレーション技術ではあまり考慮されていない流体非理想性を適切に考慮したものであり,今後の高圧燃焼流体解析技術およびそれを使用した燃焼技術の革新に資するものである.また,非理想モデルは汎用性ある形で計算ライブラリ化されており,それぞれのシミュレーションプログラムにおいて使用可能である.これにより,本研究成果の社会展開が可能である.

Report

(4 results)
  • 2019 Annual Research Report   Final Research Report ( PDF )
  • 2018 Research-status Report
  • 2017 Research-status Report
  • Research Products

    (27 results)

All 2020 2019 2018 2017

All Journal Article (4 results) (of which Peer Reviewed: 3 results,  Open Access: 2 results) Presentation (23 results) (of which Int'l Joint Research: 8 results,  Invited: 1 results)

  • [Journal Article] Fuel effects on the combustion flow structure behind a splitter plate of a rocket injector2020

    • Author(s)
      S. Murakami, H. Terashima, N. Oshima
    • Journal Title

      Aerospace Technology Japan

      Volume: -

    • NAID

      130007994889

    • Related Report
      2019 Annual Research Report
    • Peer Reviewed / Open Access
  • [Journal Article] Detailed Modeling of Supercritical Jets and Flames2020

    • Author(s)
      S. Matsuyama, H. Terashima, M. Koshi, A. Umemura
    • Journal Title

      High-Pressure Flows for Propulsion Applications, Progress in Astronautics and Aeronautics

      Volume: - Pages: 567-626

    • DOI

      10.2514/5.9781624105814.0571.0630

    • ISBN
      9781624105807, 9781624105814
    • Related Report
      2019 Annual Research Report
    • Peer Reviewed
  • [Journal Article] A localized thickened flame model: 定容容器内火炎伝播及び末端ガス自着火現象への適用2019

    • Author(s)
      寺島洋史,河合宗司
    • Journal Title

      ながれ

      Volume: 38 Pages: 435-438

    • Related Report
      2019 Annual Research Report
    • Open Access
  • [Journal Article] End-gas autoignition behaviors under pressure wave disturbance2019

    • Author(s)
      H. Terashima, A. Matsugi and M. Koshi
    • Journal Title

      Combustion and Flame

      Volume: 203 Pages: 204-216

    • DOI

      10.1016/j.combustflame.2019.02.011

    • Related Report
      2018 Research-status Report
    • Peer Reviewed
  • [Presentation] Effects of NTC region on end-gas combustion modes under temperature stratification2019

    • Author(s)
      T. Nogawa, H. Terashima
    • Organizer
      27th International Colloquium on the Dynamics, Explosions and Reactive Systems (ICDERS)
    • Related Report
      2019 Annual Research Report
    • Int'l Joint Research
  • [Presentation] Fuel effects on the combustion flow structure behind a splitter plate of a rocket injector2019

    • Author(s)
      S. Murakami, H. Terashima, N. Oshima
    • Organizer
      32nd International Symposium on Space Technology and Science (ISTS)
    • Related Report
      2019 Annual Research Report
    • Int'l Joint Research
  • [Presentation] Numerical study on cryogenic/jet crossflow interaction structures under supercritical pressure2019

    • Author(s)
      T. Amano, T. Araki, H. Terashima, D. Muto, K. Ozawa, N. Tsuboi
    • Organizer
      32nd International Symposium on Space Technology and Science (ISTS)
    • Related Report
      2019 Annual Research Report
    • Int'l Joint Research
  • [Presentation] A computational study for combustion flow fields of a high-pressure gaseous hydrogen/oxygen coflow jet behind a splitter plate2019

    • Author(s)
      S. Murakami, H. Terashima, N. Oshima
    • Organizer
      AIAA Science and Technology Forum and Exposition 2019
    • Related Report
      2019 Annual Research Report
    • Int'l Joint Research
  • [Presentation] 詳細反応機構を用いた格子依存性の少ない火炎面捕獲モデリング2019

    • Author(s)
      花田豊,河合宗司,寺島洋史
    • Organizer
      第33回数値流体力学シンポジウム
    • Related Report
      2019 Annual Research Report
  • [Presentation] 超臨界圧高密度比混合層分布の数値評価について2019

    • Author(s)
      荒木天秀,武藤大貴,寺島洋史,坪井伸幸
    • Organizer
      第33回数値流体力学シンポジウム
    • Related Report
      2019 Annual Research Report
  • [Presentation] ロケットエンジンH2/O2燃焼流れ場に対する噴射器リセス長さの影響2019

    • Author(s)
      太田徹,村上峻,寺島洋史,大島伸行
    • Organizer
      第33回数値流体力学シンポジウム
    • Related Report
      2019 Annual Research Report
  • [Presentation] 燃焼圧によるロケット噴射器近傍燃焼流れ場構造の変化:H2/O2とCH4/O2の比較2019

    • Author(s)
      村上峻,寺島洋史,大島伸行
    • Organizer
      第57回燃焼シンポジウム
    • Related Report
      2019 Annual Research Report
  • [Presentation] A localized thickened flame model: 定容容器内火炎伝播及び末端ガス自着火現象への適用2019

    • Author(s)
      寺島洋史,河合宗司
    • Organizer
      日本流体力学会年会2019
    • Related Report
      2019 Annual Research Report
  • [Presentation] 直交噴流によって誘起される爆燃爆轟波遷移現象に関する数値解析2019

    • Author(s)
      万浪義史,寺島洋史
    • Organizer
      第51回流体力学講演会/第37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
      2019 Annual Research Report
  • [Presentation] A computational study for combustion flow fields of a high-pressure gaseous hydrogen/oxygen coflow jet behind a splitter plate2019

    • Author(s)
      S. Murakami, H. Terashima, and N. Oshima
    • Organizer
      AIAA Science and Technology Forum and Exposition 2019
    • Related Report
      2018 Research-status Report
    • Int'l Joint Research
  • [Presentation] An efficient methodology for combustion flow simulations with large detailed chemical kinetics2018

    • Author(s)
      H. Terashima
    • Organizer
      Korea Society for Computational Fluids Engineering
    • Related Report
      2018 Research-status Report
    • Invited
  • [Presentation] Effects of temperature stratification on combustion modes associated with end-gas autoignition2018

    • Author(s)
      T. Nogawa and H. Terashima
    • Organizer
      Fifteenth International Conference on Fluid Dynamics
    • Related Report
      2018 Research-status Report
    • Int'l Joint Research
  • [Presentation] Comparison study of combustion flow fields and heat transfer characteristics between GCH4/GO2 single- and multi-element combustion chambers2018

    • Author(s)
      Y. Daimon, H. Negishi, H. Tani, H. Terashima, S. Silvestri, O. Haidn
    • Organizer
      Space Propulsion conference 2018
    • Related Report
      2018 Research-status Report
    • Int'l Joint Research
  • [Presentation] 非理想熱・輸送物性を考慮した超臨界圧燃焼流れシミュレーション2018

    • Author(s)
      山本賢,寺島洋史
    • Organizer
      日本機械学会北海道学生会第48回学生員卒業研究発表講演会
    • Related Report
      2018 Research-status Report
  • [Presentation] エンジン内部の温度不均一性がエンドガス自着火に与える影響2018

    • Author(s)
      野川理尚,寺島洋史
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] ロケット噴射器近傍に形成される燃焼流れ場構造:H2/O2とCH4/O2の比較2018

    • Author(s)
      村上峻,寺島洋史,大島伸行
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 超臨界圧高密度比流れに対するエネルギー/圧力発展ハイブリッド法2018

    • Author(s)
      荒木天秀,武藤大貴,寺島洋史,坪井伸幸
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] 詳細反応機構を用いたCFDにおける荒い格子上での火炎面捕獲物理モデリング2018

    • Author(s)
      高橋悠哉,寺島洋史,河合宗司
    • Organizer
      第32回数値流体力学シンポジウム
    • Related Report
      2018 Research-status Report
  • [Presentation] エネルギー/圧力発展方程式ハイブリッド法を用いた超臨界極低温噴流における密度接触面の堅牢な数値解析2018

    • Author(s)
      荒木天秀,武藤大貴,寺島洋史,坪井伸幸
    • 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] ロケット噴射器リセス長さと燃焼流れ場・性能との関係について2017

    • Author(s)
      寺島洋史,大門優
    • Organizer
      第31回数値流体力学シンポジウム
    • Related Report
      2017 Research-status Report
  • [Presentation] ロケット燃焼器における高圧メタン酸素燃焼場の解析2017

    • Author(s)
      寺島洋史,大門優,根岸秀世
    • Organizer
      日本流体力学会年会2017
    • Related Report
      2017 Research-status Report
  • [Presentation] Numerical Investigation on Effects of Recess Variation upon a GCH4/GOX Shear Coaxial Combustion Chamber2017

    • Author(s)
      Y. Daimon, H. Terashima, H. Tani, H. Negishi
    • Organizer
      31st International Symposium on Space Technology and Science (ISTS)
    • Related Report
      2017 Research-status Report
    • Int'l Joint Research

URL: 

Published: 2017-04-28   Modified: 2023-03-16  

Information User Guide FAQ News Terms of Use Attribution of KAKENHI

Powered by NII kakenhi