Search Results1-20 of  22

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  • NEGISHI HIDEYO ID: 9000402296068

    宇宙航空研究開発機構 (2010 from CiNii)

    Articles in CiNii:1

    • 第3回 極低温推進薬の高圧噴射と微粒化に関連した熱流動現象 (2010)
  • NEGISHI Hideyo ID: 9000006357601

    (独)宇宙航空研究開発機構 (2013 from CiNii)

    Articles in CiNii:5

    • 2503 Numerical Analysis for Free-surface Flows with Three-dimensional Body-fitted Grid (2005)
    • Numerical Analysis of Free-Surface Flows under Various Conditions in Acceleration : Improvement of CIP-LSM : CIP-Based Level Set & MARS(<Special Issue>The Forefront of Multi-Physics CFD/EFD) (2010)
    • (8)様々な加速度環境における自由表面流の数値解析 : CIP法, MARS法, Level Set法を協調した解法の改良(論文,日本機械学会賞〔2012年度(平成24年度)審査経過報告〕) (2013)
  • NEGISHI Hideyo ID: 9000006671385

    Japan Aerospace Exploration Agency (2015 from CiNii)

    Articles in CiNii:3

    • C1 Vertical Vibration Experiment of Concentric Membrane Tank (2007)
    • Numerical Analysis of Supercritical Hydrogen Flow in a Uniformly Heated Tube (2010)
    • Hybrid N-S/DSMC Simulations of HTV Main Engine Plume Impingement to the ISS(<Special Features>Challenges in CFD for Space Program) (2015)
  • NEGISHI Hideyo ID: 9000022061062

    Japan Aerospace Exploration Agency (JAXA) (2009 from CiNii)

    Articles in CiNii:1

    • Combustion and Regenerative Cooling Characteristics of LOX/Methane Engine (2009)
  • NEGISHI Hideyo ID: 9000296665937

    Japan Aerospace Exploration Agency (2015 from CiNii)

    Articles in CiNii:1

    • Failure mechanism and life evaluation of liquid rocket engine combustion chamber under severe multi-physics conditions (2015)
  • NEGISHI Hideyo ID: 9000305622628

    Japan Aerospace Exploration Agency (2013 from CiNii)

    Articles in CiNii:1

    • 0633 Cryogenic Hydrogen Jet in Cross-flow under Supercritical Pressure (2013)
  • NEGISHI Hideyo ID: 9000308045576

    Japan Aerospace Exploration Agency (2013 from CiNii)

    Articles in CiNii:1

    • 1211 Optical Measurements of Impinging Jet Atomization (2013)
  • NEGISHI Hideyo ID: 9000329415157

    JAXA (2015 from CiNii)

    Articles in CiNii:1

    • 179 Evaluation of high temperature and inelastic behavior of liquid rocket engine combustion chamber using thermal-fluid-structure interaction analysis (2015)
  • NEGISHI Hideyo ID: 9000380986001

    国立研究開発法人 宇宙航空研究開発機構 研究開発部門 第三研究ユニット (2018 from CiNii)

    Articles in CiNii:1

    • Report on AIAA Propulsion and Energy Forum and Exposition 2017 (2018)
  • NEGISHI Hideyo ID: 9000403402038

    Research and Development Directorate, Japan Aerospace Exploration Agency (2019 from CiNii)

    Articles in CiNii:1

    • Numerical analysis of dam breaking behavior of Bingham pseudoplastic fluid by using the explicit MPS method (2019)
  • NEGISHI Hideyo ID: 9000404541284

    (国研)宇宙航空研究開発機構 研究開発部門 第三研究ユニット (2018 from CiNii)

    Articles in CiNii:1

    • Investigation on Flow Field Characteristics of a Liquid Rocket Open Impeller Based on Compressible URANS Simulation (2018)
  • NEGISHI Hideyo ID: 9000409478506

    Japan Aerospace Exploration Agency (2019 from CiNii)

    Articles in CiNii:1

    • High-Fidelity Contact Force Modeling for the Spacecraft Docking and Capturing Systems (2019)
  • NEGISHI Hideyo ID: 9000409858429

    宇宙航空研究開発機構(JAXA) (2020 from CiNii)

    Articles in CiNii:1

    • CFD-based Aerothermodynamics Design for HTV Small Re-entry Capsule Project (2020)
  • NEGISHI Hideyo ID: 9000409858443

    宇宙航空研究開発機構 研究開発部門第三研究ユニット (2020 from CiNii)

    Articles in CiNii:1

    • Overview and Outlook of Information and Computational Engineering Technology in Support of Space Development (2020)
  • NEGISHI Hideyo ID: 9000410514645

    Research and Development Directorate, Japan Aerospace Exploration Agency (2020 from CiNii)

    Articles in CiNii:1

    • Numerical analysis of fluid lubrication in line contact by using the MPS method (2020)
  • Negishi Hideyo ID: 9000003848838

    Dept. of Mechanical and Aerospace Engineering, Tokyo Institute of Technology (2001 from CiNii)

    Articles in CiNii:1

    • F-1521 Numerical Simulations of Boat-tail Drag Reduction (2001)
  • Negishi Hideyo ID: 9000318134581

    Japan Aerospace Exploration Agency (2015 from CiNii)

    Articles in CiNii:1

    • Toward the Understanding of Mixing and Combustion Characteristics of Hypergolic Propellants for Spacecraft Thrusters(<Special Features>Challenges in CFD for Space Program) (2015)
  • Negishi Hideyo ID: 9000329417534

    JAXA (2015 from CiNii)

    Articles in CiNii:1

    • 120 Coupled Thermal-Fluid Simulation for Predicting Regenerative Cooling Performance in Liquid Rocket Engine Combustion Chambers (2015)
  • Negishi Hideyo ID: 9000329417550

    Japan Aerospace Exploration Agency (2015 from CiNii)

    Articles in CiNii:1

    • 127 Reentry Capsule Cover Separation Motion CFD Analysis with Uncertainties (2015)
  • Negishi Hideyo ID: 9000408812543

    Articles in CiNii:1

    • Interface Tracking Simulations of Liquid Rocket Engine Combustion at Subcritical Pressures (2016)
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