山根 敬 YAMANE Takashi

Articles:  1-20 of 35

  • 1 / 2
  • Numerical Simulation of High Temperature and High Speed Gas-Solid Two-Phase Flow  [in Japanese]

    鈴木 正也 , 山根 敬

    日本ガスタービン学会定期講演会講演論文集 45, 271-275, 2017-10-18

  • Study on the Influence of Re-heating as a Supersonic Propulsion System  [in Japanese]

    福山 佳孝 , 山根 敬

    日本ガスタービン学会定期講演会講演論文集 45, 89-94, 2017-10-18

  • Application of numerical simulation technology to aero engine development in JAXA  [in Japanese]

    MAKIDA Mitsumasa , HOJO Masahiro , KITAMURA Yoshihiro , YAMANE Takashi , KAZAWA Jyunichi , SUZUKI Masaya , NISHIZAWA Toshio

    Journal of the Gas Turbine Society of Japan 43(6), 414-421,図巻頭1p, 2015-11

  • International Conferences on Gas Turbines and Jet Engines  [in Japanese]

    NAKAMATA Chiyuki , OKAI Keiichi , KODAMA Hidekazu , GOTO Jinichiro , YAMANE Takashi , YAMAMOTO Makoto , OKI Yuso , HAMADA Hiroyuki , MIYAGAWA Kazuyoshi , MIYOSHI Ichiro

    Journal of the Gas Turbine Society of Japan 43(1), 8-13, 2015-01

  • C-21 Unsteady Full-Annular Simulation of Fan-Bypass Duct Flow  [in Japanese]

    NOZAKI Osamu , YAMANE Takashi , KUSUDA Shinya , OOBA Yoshinori , ISHIYAMA Takeshi

    It is important to improve the installation loss due to the interaction fan/OGV/strut/pylon of gas-turbine engines. Researches on numerical simulation using unsteady CFD analyses were conducted to pre …

    ガスタービン定期講演会講演論文集 (41), 375-380, 2013-10-16

  • Asian Congress on Gas Turbines 2012報告  [in Japanese]

    YAMANE Takashi

    Journal of the Gas Turbine Society of Japan 40(6), 374-377, 2012-11

  • CFD Application to Aircraft Gas Turbines at JAXA  [in Japanese]

    NOZAKI Osamu , KAZAWA Junichi , MAKIDA Mitsumasa , YAMANE Takashi , ENOMOTO Shunji

    Journal of the Gas Turbine Society of Japan 40(6), 274-281,図巻頭1p, 2012-11

    Cited by (1)

  • C-25 Structure Change of Single Crystal Superalloy under Cyclic Thermal Stress with Mechanical Stress  [in Japanese]

    YAMANE Takashi , AOKI Ryota , FUKUYAMA Yoshitaka

    In order to evaluate structure changes of single crystal superalloy under the simulated condition of jet engine operations, new test equipment which also adds tensile stress as well as cyclic thermal …

    ガスタービン定期講演会講演論文集 (40), 337-340, 2012-10-17

  • Numerical Simulation Technologies on Heat Transfer Problems in Aeroengines  [in Japanese]

    YAMANE Takashi

    Journal of the Gas Turbine Society of Japan 38(3), 166-173, 2010-05-20

    References (42)

  • On Accuracy Improvement of Conjugate Heat Transfer Analysis  [in Japanese]

    BAMBA Takahiro , YAMANE Takashi , FUKUYAMA Yoshitaka

    タービン翼等の高温部材に適用する高性能冷却構造体の開発には、熱負荷分布の詳細な予測が欠かせない。これを容易に行う解析手法としてUPACS を利用した流体・熱伝導連成解析手法の開発に取り組んでいる。流体と同時に流体と接する物体内部の熱伝導も解く手法であり、壁面の温度境界条件を陽に与える必要が無く、部材内部の温度場も解析できるため、高温部材の熱解析には非常に有用な手法である。本報では、連成解析の流体部 …

    JAXA research and development report JAXA-RR-07-031, 1-14, 2008-02

  • B-2 Conjugate Simulation on Film Cooling  [in Japanese]

    BABA Takahiro , TANAKA Kouhei , YAmANE Takahis , FUKUYAMA Yoshitaka , YOSHIDA Toyoaki

    Numerical simulations were performed to study the film cooling of a flat plate with simple internal convective cooling with and without the account for the heat transfer in the solid. The aim of the p …

    ガスタービン定期講演会講演論文集 (35), 125-130, 2007-09-01

  • B-1 Study of Cooling Effectiveness for an Integrated Cooling  [in Japanese]

    MATSUSHITA Masahiro , YAMANE Takashi , MIMURA Fujio , FUKUYAMA Yoshitaka

    Experimental study of film cooling, impingement cooling, integrated cooling were carried out with the aim of applying them to turbine cooling. The experiments were conducted with 673K hot gas flow and …

    ガスタービン定期講演会講演論文集 (35), 119-124, 2007-09-01

  • Numerical Analysis on Turbine Heat Transfer  [in Japanese]

    YAMANE Takashi

    Journal of the Gas Turbine Society of Japan 35(3), 182-187, 2007-05-20

    References (31) Cited by (1)

  • Study of Cooling Effectiveness for an Integrated Cooling Turbine Blade  [in Japanese]

    MATSUSHITA Masahiro , YAMANE Takashi , MIMURA Fujio , FUKUYAMA Yoshitaka

    タービン翼の冷却研究目的で,フィルム冷却,インピンジメント冷却の基礎実験,および,それら組み合わせた複合冷却の実験を実施した.実験は673K の燃焼ガスに対し室温の冷却空気を使用し,試験体表面の温度計測は赤外線カメラによって行った.これら,基礎的な実験データはCFD などの解析へ利用することを念頭においており,本報告では,基本的な各冷却構造の試験結果,各冷却構造を組み合わせた複合冷却の基礎試験結果 …

    JAXA research and development report JAXA-RR-06-027, 1-54, 2007-03

  • A-5 Experimental Research on Cooling Performance of an Innovative Cooling Structure-Multiple Angled Impingement  [in Japanese]

    Fujimoto Shu , Okita Yoji , Fukuyama Yoshitaka , Yamane Takahsi , Mimura Fujio , Matsushita Masahiro , Yoshida Toyoaki

    Innovative cooling method named Multiple Angled Impingement, which realizes drastic reduction of cooling air used for turbine shrouds, has been invented. To confirm cooling performance of this cooling …

    ガスタービン定期講演会講演論文集 (34), 35-39, 2006-10-01

  • Cooling Effectiveness Distribution of an Integrated Impingement and Pin Fin Cooling Configuration  [in Japanese]

    NAKAMATA Chiyuki , MIMURA Fujio , MATSUSHITA Masahiro , YAMANE Takashi , FUKUYAMA Yoshitaka , YOSHIDA Toyoaki

    Experimental study was conducted for the development of the integrated impingement and pin-fin cooling configuration. The temperature measurements were performed for different test pieces with various …

    Journal of the Gas Turbine Society of Japan 34(5), 363-368, 2006-09-20

    References (5)

  • Pin Arrangement Dependence of Cooling Performance of an Integrated Impingement and Pin Fin Cooling Configuration  [in Japanese]

    NAKAMATA Chiyuki , OKITA Yoji , MIMURA Fujio , MATSUSHITA Masahiro , YAMANE Takashi , FUKUYAMA Yoshitaka , YOSHIDA Toyoaki

    Experimental study was conducted for the development of the integrated impingement and pin-fin cooling configuration. In the development, the spatial arrangements of impingement holes, pin-fins and fi …

    Journal of the Gas Turbine Society of Japan 34(2), 112-117, 2006-03-20

    References (6) Cited by (1)

  • アジアガスタービン会議(ACGT 2005)報告  [in Japanese]

    YAMANE Takashi

    Journal of the Gas Turbine Society of Japan 34(1), 67-69, 2006-01-20

  • A-3 Influences of Turbulence Models on 2D Cascade Heat Transfer Using the Conjugate Simulation of Flow and Heat Conduction  [in Japanese]

    BAMBA Takahiro , YAMANE Takashi , FUKUYAMA Yoshitaka

    In flow simulation with large strain rate, the selection of turbulence model gives unignorable influence on heat transfer prediction, which is known as the stagnation anomaly. Typical turbine cascade …

    第34回ガスタービン定期講演会講演論文集, 2006, 25-30, 2006

    Cited by (1)

  • B-11 Influences of Turbulence Models on Impingement Cooling Using the Conjugate Simulation of Flow and Heat Transfer  [in Japanese]

    BAMBA Takahiro , IMAMURA Taro , YAMANE Takashi , FUKUYAMA Yoshitaka

    A series of numerical simulations of single impingement cooling jet were conducted on UPACS, a common CFD platform developed in JAXA, with three different RANS turbulence models (Spalart-Allmaras, k-ω …

    ガスタービン定期講演会講演論文集 (33), 165-168, 2005-09-01

  • 1 / 2
Page Top