Search Results1-13 of  13

  • KUROTAKI Takuji ID: 9000000810066

    航空宇宙技術研究所流体科学研究センター (2002 from CiNii)

    Articles in CiNii:1

    • 壁面触媒性を考慮した非平衡流における空力加熱特性について (2002)
  • KUROTAKI Takuji ID: 9000001491401

    The Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (2006 from CiNii)

    Articles in CiNii:2

    • Numerical Simulation of Inductively Coupled Air Plasmas (2005)
    • Oxygen Recombination Coefficient on Catalytic Surfaces in Ar-O_2 Inductively Coupled Plasma by Actinometry (2006)
  • KUROTAKI Takuji ID: 9000002626297

    National Aerospace Laboratory (2003 from CiNii)

    Articles in CiNii:1

    • A Study on High Temperature Effects in Shock Wave/Boundary Layer Interaction Induced by Compression Corner (2003)
  • KUROTAKI Takuji ID: 9000003846016

    NAL (2002 from CiNii)

    Articles in CiNii:4

    • Aeroelastic Analysis of the Non-powered Supersonic Experimental Aircraft with Elastic Deformation (2002)
    • Flow around OREX and Estimation of Aerodynamic Heat (2002)
    • Finite Rate Catalytic Effects of Reentry Vehicles (2001)
  • KUROTAKI Takuji ID: 9000017013071

    宇宙航空研究開発機構総合技術研究本部 (2005 from CiNii)

    Articles in CiNii:3

    • Static Pressure Measurement of High Enthalpy Flow in Arc-Heated Wind Tunnel (2002)
    • Numerical Simulation of Inductively Coupled Air Plasmas (2005)
    • 750kWアーク加熱風洞気流の圧力計測 (2002)
  • KUROTAKI Takuji ID: 9000018330430

    宇宙航空研究開発機構研究開発本部 (2009 from CiNii)

    Articles in CiNii:4

    • Construction of Generalized Characteristic Interface Conditions for High-Order Multi-Block Fluid Computation and Its Performance Evaluation (2006)
    • Multi-Block Computation by Characteristic Interface Conditions with High-Order Interpolation (2009)
    • AM06-11-006 Accurate simulation of boundary-layer transition by an advanced LES (2006)
  • KUROTAKI Takuji ID: 9000022060607

    Japan Aerospace Exploration Agency, Institute of Space Technology and Aeronautics (2005 from CiNii)

    Articles in CiNii:1

    • Numerical Simulation of Inductively Coupled Air Plasmas (2005)
  • KUROTAKI Takuji ID: 9000253509253

    NAL (2002 from CiNii)

    Articles in CiNii:1

    • Aeroelastic Analysis of the Non-powered Supersonic Experimental Aircraft with Elastic Deformation (2002)
  • KUROTAKI Takuji ID: 9000254356817

    The Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (2003 from CiNii)

    Articles in CiNii:1

    • Precise Method to Estimate Aerodynamic Heat on Reentry Vehicles while Atmospheric Reentry (2003)
  • KUROTAKI Takuji ID: 9000258441608

    JAXA/IAT (2008 from CiNii)

    Articles in CiNii:1

    • A numerical study of the acoustic noise generation from a 2-D airfoil at a low Reynolds number (2008)
  • KUROTAKI Takuji ID: 9000402388385

    Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (2019 from CiNii)

    Articles in CiNii:1

    • Preliminary study on compressible gas-liquid two-phase flow computation for ultra-high-pressure fuel injection process (2019)
  • Kurotaki Takuji ID: 9000002568253

    航空宇宙技術研究所 (1998 from CiNii)

    Articles in CiNii:6

    • Numerical Analysis of Two Dimensional / Axisymmetric Non-equilibrium Hypersonic Flow(Proceedings of the 10th NAL Smposium on Aircraft Computational Aerodynamics) (1992)
    • Numerical Analysis of Non-equilibrium Hypersonic Flow around Reentry Vehicle(Proceedings of the 12th NAL Symposium on Aircraft Computational Aerodynamics. CFD Workshop on Hypersonic Flow) (1994)
    • Numerical Simulation of Film Cooling Effect around Axisymmetric Body in Hypersonic Flow Field(Proceedings of the 12th NAL Symposium on Aircraft Computational Aerodynamics) (1994)
  • Kurotaki Takuji ID: 9000002568583

    航空宇宙技術研究所 (1996 from CiNii)

    Articles in CiNii:1

    • Numerical Analysis of Thermochemical Nonequilibrium Hypersonic Flow around Blunt Body(Proceedings of the 13th NAL Symposium on Aircraft Computational Aerodynamics. High Enthalpy Flow Organized Session and Workshop) (1996)
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