Search Results1-20 of  44

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  • 青山 剛史 ID: 9000241863015

    Articles in CiNii:1

    • An anisotropic constitutive relation of the Reynolds stresses for numerical simulations of three-dimensional wall jets (2013)
  • 青山 剛史 ID: 9000246807682

    Articles in CiNii:1

    • Validation of fundamental sound transmission analysis by the hybrid finite element-wave based method (2014)
  • 青山 剛史 ID: 9000291607177

    Articles in CiNii:1

    • Development of Nonlinear Acoustic Propagation Analysis Tool toward Realization of Laud Noise Prediction in Aeronautics and Space (2015)
  • 青山 剛史 ID: 9000323833794

    Articles in CiNii:1

    • First Report of High Speed Model Helicopter Flight Test (2016)
  • 青山 剛史 ID: 9000323834300

    Articles in CiNii:1

    • 遷音速バフェットにおける後退角効果 (2016)
  • 青山 剛史 ID: 9000383220319

    Articles in CiNii:1

    • A Study on Spreading Wakes by Wind Turbine Wake Simulation (2017)
  • 青山 剛史 ID: 9000390400021

    Articles in CiNii:1

    • Development of Fast Unstructured-Grid Flow Solver (2018)
  • 青山 剛史 ID: 9000397936678

    Articles in CiNii:1

    • Development of Large-scale Dynamic Fluid-Body Interaction Simulation Technology for Multi-body Collision Avoidance Study (2018)
  • 青山 剛史 ID: 9000399350654

    Articles in CiNii:1

    • Numerical analysis of wind distributions in wind turbine wake (2017)
  • 青山 剛史 ID: 9000402488947

    Articles in CiNii:1

    • Numerical Simulation of Flow Around a Slat Using Embedded-LES Method (2019)
  • 青山 剛史 ID: 9000402767572

    Articles in CiNii:1

    • Practical Application of Large-scale Unsteady CFD Analysis for Aircraft Design (2019)
  • 青山 剛史 ID: 9000402930112

    Articles in CiNii:1

    • 基礎・基盤技術(2)数値解析技術 コンピュータの中に自然現象を再現する技術 (2019)
  • 青山 剛史 ID: 9000403288089

    Articles in CiNii:1

    • BVI Noise of Helicopter and Its Prediction Method (2019)
  • AOYAMA TAKASHI ID: 9000258440961

    Japan Aerospace Exploration Agency (JAXA) (2007 from CiNii)

    Articles in CiNii:1

    • Effect of tip vortices decay on the prediction of helicopter BVI noise (2007)
  • AOYAMA TAKASHI ID: 9000258441616

    Japan Aerospace Exploration Agency (JAXA) (2008 from CiNii)

    Articles in CiNii:1

    • Numerical analysis of sound generation by flapping wings (2008)
  • AOYAMA TAKASHI ID: 9000283784477

    Japan Aerospace Exploration Agency (2004 from CiNii)

    Articles in CiNii:1

    • Aerodynamic analysis of rotor higher harmonic control using a CFD technique (2004)
  • AOYAMA Takashi ID: 9000002568003

    Numerical Analysis Group, Aerospace Research and Development Directorate (2009 from CiNii)

    Articles in CiNii:22

    • On Helicopter Noise-From the Viewpoint of Impulsive Noise (1995)
    • Numerical Optimization for Generating Low-boom Pressuter Signatures (1997)
    • Control of Helicopter Rotor Noise (2000)
  • AOYAMA Takashi ID: 9000006819831

    宇宙航空研究開発機構 (2013 from CiNii)

    Articles in CiNii:13

    • Computational Research on Vibro-Acoustics at Rocket Launch (2007)
    • Numerical Analysis and Visualization of Sound Transmission to Solid (2009)
    • Large-Deformation Aeroelastic Analysis Using Fluid-Structure Coupled Method (2010)
  • AOYAMA Takashi ID: 9000014562639

    Computational Science Research Group, Institute of Aerospace Technology (2008 from CiNii)

    Articles in CiNii:2

    • Prediction of Helicopter BVI Noise Considering Blade Elastic Deformation and Tip Vortex Decay (2008)
    • Comprehensive Study on Interpolation Methods for Helicopter Simulation : Interpolation between Cartesian and Curvilinear Grids in Parallel Computation (2008)
  • AOYAMA Takashi ID: 9000015629289

    航空宇宙技術研究所 流体科学研究センター (2003 from CiNii)

    Articles in CiNii:1

    • Prediction Methods ofHelicopter High Speed Impulsive Noise Using CFD (2003)
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