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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
関連記事はまだありません。
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1.
Boiling induced atomization of liquid film produced by oblique jet impingement on superheated wall
Noritaka Sako; Jun Hayashi; Chihiro Inoue; Hiroshi KawanabeYu Daimon
Experimental Thermal and Fluid Science 158: 111262 (2024) Semantic Scholar
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2.
Liquid film and heat transfer characteristics during superheated wall cooling via pulsed injection of a liquid jet
Noritaka Sako; Kouhei Noda; Jun Hayashi; Yu DaimonHiroshi Kawanabe
International Journal of Heat and Mass Transfer 205: (2023) Semantic Scholar
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3.
Scattering Tendency of Surface Objects during Thrusting in Vicinity of Celestial Body
Maiko YAMAKAWA; Yusuke MARU; Mitsuhisa BABA; Yu DAIMON (+3 著者) Yuichi TSUDA
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 21: 29 (2023) Semantic Scholar
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4.
Quenching of a heated wall with spatial temperature gradient using a liquid film through oblique jet impingement
Noritaka Sako; Kouhei Noda; Jun Hayashi; Daimon YuHiroshi Kawanabe
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER 192: (2022) Semantic Scholar
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5.
Evaporation of Three-Dimensional Wavy Liquid Film Entrained by Turbulent Gas Flow
Takuya Inoue; Chihiro Inoue; Go Fujii; Yu Daimon
AIAA JOURNAL 60: 3805 (2022)
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6.
Visualization of Coolant Liquid Film Dynamics in Hypergolic Bipropellant Thruster
Go Fujii; Yu Daimon; Katsumi Furukawa; Chihiro Inoue (+1 著者) Nobuhiko Tanaka
JOURNAL OF PROPULSION AND POWER 38: 267 (2022) Semantic Scholar
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7.
Direct Formulation of Bipropellant Thruster Performance for Quantitative Cold-Flow Diagnostic
Chihiro Inoue; Yuki Oishi; Yu Daimon; Go FujiiKaname Kawatsu
JOURNAL OF PROPULSION AND POWER 37: 842 (2021) Semantic Scholar
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8.
Boiling induced atomization appeared in the liquid film by wall impinging jet on the superheated wall
Noritaka Sako; Jun Hayashi; Chihiro Inoue; Hiroshi KawanabeYu Daimon
ICLASS 2021 - 15th Triennial International Conference on Liquid Atomization and Spray Systems (2021)
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9.
Wall modeling of turbulent methane/oxygen reacting flows for predicting heat transfer
Daiki Muto; Yu Daimon; Hideyo Negishi; Taro Shimizu
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW 87: (2021) Semantic Scholar
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10.
Experimental analysis of the spreading of a liquid film on a bipropellant thruster chamber wall
Noritaka Sako; Jun Hayashi; Yu Daimon; Hiroumi TaniHiroshi Kawanabe
JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY 16: (2021) Semantic Scholar
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11.
Visualization of Pulse Firing Mode in Hypergolic Bipropellant Thruster
Go Fujii; Yu Daimon; Chihiro Inoue; Daijiro Shiraiwa (+1 著者) Katsumi Furukawa
JOURNAL OF PROPULSION AND POWER 36: 677 (2020) Semantic Scholar
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12.
Experimental study on cryo-compressed hydrogen ignition and flame
Hiroaki Kobayashi; Daiki Muto; Yu Daimon; Yutaka Umemura (+4 著者) Kota Miyanabe
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 45: 5098 (2020) Semantic Scholar
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13.
Proposal of Specific Impulse Prediction Method for Bipropellant Thrusters
Yuto Terauchi; Chihiro Inoue; Yu Daimon; Go Fujii
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 63: 189 (2020) Semantic Scholar
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14.
An equilibrium wall model for reacting turbulent flows with heat transfer
Daiki Muto; Yu Daimon; Taro Shimizu; Hideyo Negishi
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER 141: 1187 (2019) Semantic Scholar
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15.
Multilayer reaction zones of a counterflow flame of gaseous Nitrogen Tetroxide and a liquid Monomethylhydrazine pool
Jun Hayashi; Hiroumi Tani; Nozomu Kanno; Daisuke Sato (+4 著者) Timothee Pourpoint
COMBUSTION AND FLAME 201: 244 (2019) Semantic Scholar
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16.
異種衝突噴霧の流管モデルに基づく二液スラスタ性能予測 : フィルム冷却燃料の効果—Bi-Propellant Thruster Performance Prediction Based on Stream Tube Model at Unlike Impinging Spray : Effect of Film Cooling Fuel
井上 智博; 藤井 剛; 大門 優
微粒化 = Atomization : journal of the ILASS-Japan 28: 11 (2019)
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17.
Observation of Electron Density Depletion Due to Maneuver Operation of H‐II Transfer Vehicle
T. Okumura; D. Tsujita; H. Tani; Y. Daimon (+4 著者) H. Okamoto
Journal of Geophysical Research: Space Physics 124: 2238 (2019) Semantic Scholar
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18.
Unified Length Scale of Spray Structure by Unlike Impinging Jets
Chihiro Inoue; Yuta Takeuchi; Koji Nozaki; Takehiro Himeno (+2 著者) Yu Daimon
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 62: 213 (2019) Semantic Scholar
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19.
Temperature measurement and flow visualization of cryo-compressed hydrogen released into the atmosphere
Hiroaki Kobayashi; Yu Daimon; Yutaka Umemura; Daiki Muto (+1 著者) Kota Miyanabe
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 43: 17938 (2018) Semantic Scholar
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20.
A Numerical Study on Hypergolic Combustion of Hydrazine Sprays in Nitrogen Tetroxide Streams
Hiroumi Tani; Hiroshi Terashima; Yu Daimon; Mitsuo KoshiRyoichi Kurose
COMBUSTION SCIENCE AND TECHNOLOGY 190: 515 (2018) Semantic Scholar
書籍等出版物情報はまだありません。
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61.
Flowfield and heat transfer characteristics in the LE-X expander bleed cycle combustion chamber
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014 2014年
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62.
Numerical and Experimental Investigation of the Methane Film Cooling in Subscale Combustion Chamber
5th European Conference for Aeronautics and Space Sciences 2013年7月
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63.
An order estimation of the acoustic losses inside a simulated liquid rocket chamber
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2013年
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64.
Design verification results of Japanese 120N Bi-propellant thrusters (HBT-1) based on its first flight in HTV3
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2013年
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65.
Cooling analysis for rocket engine combustion chamber with high fidelity simulation
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2013年
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66.
Conjugated combustion and heat transfer modeling for full-scale regeneratively cooled thrust chambers
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2013年
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67.
Chemical kinetics of hypergolic ignition in hydrazine/nitrogen-dioxide gas mixtures
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013 2013年
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68.
Flowfield and Heat Transfer Characteristics of Cooling Channel Flows in a Methane-Cooled Thrust Chamber
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2012年7月30日 American Institute of Aeronautics and Astronautics
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69.
Flowfield and heat transfer characteristics of a GH2/LOX calorimeter chamber with multi-injector elements
Space Propulsion 2012 2012年
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70.
Combustion and heat transfer modeling in regeneratively cooled thrust chambers (optimal solution procedures for heat flux estimation of a full-scale thrust chamber)
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012 2012年
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71.
Flowfield and heat transfer characteristics of cooling channel flows in a methane-cooled thrust chamber
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012 2012年
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72.
Acoustic structure and damping estimation of a cylindrical rocket chamber during oscillation
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012 2012年
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73.
Flowfield and Heat Transfer Characteristics of Cooling Channel Flows in a Subscale Thrust Chamber
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2011年7月31日 American Institute of Aeronautics and Astronautics
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74.
An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Risk Mitigation Study of Turbine Blade Break off
4TH EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS) 2011年7月
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75.
Evaluation of Rate Constants Relevant to the Hypergolic Reaction of Hydrazine with Nitrogen Dioxide
Seventh Mediterranean Combustion Symposium 2011年
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76.
Slit resonator design and damping estimation in linear and non-linear ranges
41st AIAA Fluid Dynamics Conference and Exhibit 2011年
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77.
Combustion and heat transfer modeling in regeneratively cooled thrust chambers (multi-injecton flow features)
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 2011年
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78.
Studies on combustion instability for liquid propellant rocket engines
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 2011年
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79.
Combustion instability phenomena observed during cryogenic hydrogen injection temperature ramping tests for single coaxial injector elements
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 2011年
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80.
An end-to-end high fidelity numerical simulation of the LE-X Engine - Engine performance evaluation and risk mitigation study -
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 2011年
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