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大門 優

Daimon, Yu

研究開発部門 , 研究開発員
Reserach and Development Directrate , Researcher

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  1. 1. Laminar Diffusion Flame-holding Characteristics in Cross-flow Formed at the Wake of the Injector Post
    AIAA SCITECH 2023 Forum 2023年1月19日
  2. 2. Heat Transfer Characteristics of Liquid Film Formed on a Superheated Wall during Pulsed Injection of Liquid Jet
    AIAA SCITECH 2023 Forum 2023年1月19日
  3. 3. Tendency of Regolith Dispersal by Firing Multiple Thrusters of Spacecraft on Celestial Surface
    International Astronautical Congress 2022 2022年9月
  4. 4. On-Orbit Test of Exhaust Gas Plume and Validation of A Hybrid Navier-Stokes/DSMC Simulation for Plume Impingement
    8th Edition of the Space Propulsion Conference 2022年5月
  5. 5. Visualization of Hard Start Phenomena in Hypergolic Bipropellant Thrusters
    8th Edition of the Space Propulsion Conference 2022年5月
  6. 6. Development of a Dynamic Response Model Considering Trapped Gas Effect for Spacecraft Liquid Propulsion Systems
    33rd International Symposium on Space Technology and Science 2022年2月
  7. 7. Scattering tendency of a surface object during thrusting in the vicinity of a celestial body
    33rd International Symposium on Space Technology and Science 2022年2月
  8. 8. Evaporation of Three-Dimensional Wavy Liquid Film Entrained by Turbulent Gas Flow
    AIAA Propulsion and Energy 2021 Forum 2021年8月9日 American Institute of Aeronautics and Astronautics
  9. 9. Numerical investigation on combustion modes of impinging hypergolic propellants
    The 10th Asian Joint Conference on Propulsion and Power 2021年3月
  10. 10. Verification of the scattering mechanism of celestial surface objects by thruster injection
    Proceedings of the International Astronautical Congress, IAC 2021年
  11. 11. Verification of the Transient Behavior of the SLIM Propulsion System (Smart Lander for Investigating Moon)
    AIAA Propulsion and Energy Forum, 2021 2021年
  12. 12. Resilient Redundant Spacecraft GN&C System Fault Detection and Diagnostics
    Aerospace Europe Conference 2020 2020年2月
  13. 13. Prediction of pressure loss in injector for rotating detonation engines using single-element simulations
    AIAA Propulsion and Energy 2020 Forum 2020年
  14. 14. Direct formulation and quantitative water-flow diagnostic for bi-propellant thruster performance
    AIAA Propulsion and Energy 2020 Forum 2020年
  15. 15. Visualization of Liquid Film for Film Cooling Formed on Combustion Chamber Wall of Bipropellant Thruster
    The 2nd Pacific Rim Thermal Engineering Conference 2019年12月
  16. 16. Wall-Modeled Large Eddy Simulation For Predicting Wall Heat Flux In A Rocket Combustion Chamber
    8th European Conference for Aeronautics and Space Sciences 2019年7月
  17. 17. Engine Re-Start Transient Simulation Tool For Cryogenic Liquid Rocket System
    8th European Conference for Aeronautics and Space Sciences 2019年7月
  18. 18. System-level Integrated Modeling and Simulation Targeting Space Propulsion System for Design Evaluation and Risk Assessment
    2nd International Symposium on Space Technology and Science 2019年6月
  19. 19. Study on Chemical Heat Sink of N-Dodecane under Supercritical Condition
    32nd International Symposium on Space Technology and Science 2019年6月
  20. 20. Large eddy simulation of mixing and combustion in a multi-element GOX/GCH4 rocket chamber
    32nd International Symposium on Space Technology and Science 2019年6月
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