Daimon Yu

ダイモンユウ | Daimon Yu

Affiliation and department：
Job title： Researcher

Research field (2)： Thermal engineering , Fluid engineering

Research keywords (6)： CFD , Combustion Simulation , 希薄流体解析 , Multi phase flow , ロケット , Detonation

Research theme for competitive and other funds (9)：

2022 - 2025 Study on three-dimensional film cooling flow heated by turbulent flow for spacecraft engine heat management
2017 - 2022 Development of explosion safety evaluation technology for liquid hydrogen using rocket engine combustion symulation method
2019 - 2019 Combustion Modeling Study for GCH4/LOX and GCH4/GOX Single Element Combustion Chambers
2014 - 2017 Study of Ignition Process on Hypergolic Fuel Using Detailed Chemical Reaction Model Constraction and High Time Resolution Non-contact Measurement
2017 - 2017 Combustion Modeling Study for a GOX-GCH4 Multi-element Combustion Chamber

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Papers (40)：

Noritaka Sako, Kouhei Noda, Jun Hayashi, Yu Daimon, Hiroshi Kawanabe. Liquid film and heat transfer characteristics during superheated wall cooling via pulsed injection of a liquid jet. International Journal of Heat and Mass Transfer. 2023. 205
Noritaka Sako, Kouhei Noda, Jun Hayashi, Daimon Yu, Hiroshi Kawanabe. Quenching of a heated wall with spatial temperature gradient using a liquid film through oblique jet impingement. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER. 2022. 192
Takuya Inoue, Chihiro Inoue, Go Fujii, Yu Daimon. Evaporation of Three-Dimensional Wavy Liquid Film Entrained by Turbulent Gas Flow. AIAA JOURNAL. 2022. 60. 6. 3805-3812
Go Fujii, Yu Daimon, Katsumi Furukawa, Chihiro Inoue, Daijiro Shiraiwa, Nobuhiko Tanaka. Visualization of Coolant Liquid Film Dynamics in Hypergolic Bipropellant Thruster. JOURNAL OF PROPULSION AND POWER. 2022. 38. 2. 267-273
Chihiro Inoue, Yuki Oishi, Yu Daimon, Go Fujii, Kaname Kawatsu. Direct Formulation of Bipropellant Thruster Performance for Quantitative Cold-Flow Diagnostic. JOURNAL OF PROPULSION AND POWER. 2021. 37. 6. 842-849

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MISC (1)：

Daimon Yu, Daimon Yu, Daimon Yu, Toru Shimada, Toru Shimada, Toru Shimada, Nobuyuki Tsuboi, Nobuyuki Tsuboi, Nobuyuki Tsuboi, Kazuhisa Fujita, et al. Predictions of nozzle shape change using a coupled fluid/thermochemical approach. Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference. 2007. 8. 7662-7670

Lectures and oral presentations (107)：

Tendency of Regolith Dispersal by Firing Multiple Thrusters of Spacecraft on Celestial Surface
(International Astronautical Congress 2022 2022)
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)
Visualization of Hard Start Phenomena in Hypergolic Bipropellant Thrusters
(8th Edition of the Space Propulsion Conference 2022)
Development of a Dynamic Response Model Considering Trapped Gas Effect for Spacecraft Liquid Propulsion Systems
(33rd International Symposium on Space Technology and Science 2022)
Scattering tendency of a surface object during thrusting in the vicinity of a celestial body
(33rd International Symposium on Space Technology and Science 2022)

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Education (1)：

Professional career (1)：

Work history (5)：

2012/04 - 現在 Japan Aerospace Exploration Agency
2011/04 - 2014/03 The University of Tokyo
2008/08 - 2012/03 Japan Aerospace Exploration Agency
2007/01 - 2008/08 University of Illinois at Urbana-Champaign Center for the Simulation of Advanced Rockets Postdoctoral Research Associate
2005/04 - 2007/01 Japan Aerospace Exploration Agency Institute of Space and Astronautical Science

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