All Stories

  1. Fluid–rigid body coupling simulations with the passively moving solid model based on a physically consistent particle method

    Article • Physics of Fluids, March 2024, American Institute of Physics

    Hideyo Negishi

  2. Numerical Study of Tip Clearance Effects in a Centrifugal Pump with Unshrouded Impeller for Liquid Rocket Engines

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  3. Conjugated Combustion and Heat Transfer Simulations of Upper and Lower Main Combustion Chambers of LE-9 Engine

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  4. Computatonal Analysis of Supercritical and Transcritical Flow in Cooling Channels with Rough Surface

    Article • July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  5. Numerical Analysis of Unshrouded Impeller Flowfield in the LE-X Liquid Hydrogen Pump

    Article • July 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  6. Numerical Investigation of Longer Life Combustion Chambers of Liquid Rocket Engines Based on Coupled Thermal-fluid-structure Simulation

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Mr. Shusuke Hori, Hideyo Negishi

  7. Validation of LS-FLOW for Reentry Capsule Unsteady Aerodynamic Analysis

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  8. Experimental Investigation on Liquid Acquisition Devices by Mesh-type Baffles

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  9. Regenerative Cooling Performance Analysis of the LE-X Engine Combustion Chamber

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  10. Numerical Modeling of Boiling Flow in a Cryogenic Propulsion System

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi

  11. Sounding Rocket Experiment on Chill-down Process with Liquid Nitrogen in a Complex Channel

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Koichi Okita, Hideyo Negishi

  12. Flowfield and Heat Transfer Characteristics in the LE-X Expander Bleed Cycle Combustion Chamber

    Article • July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hideyo Negishi