ホーム > 大門 優/ Daimon, Yu
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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101.
Detailed Features of Wave Structure and Unsteadiness on Shock-Induced Combustion and Stabilized Oblique Detonation around Hypersonic Projectile
31st International Symposium on Combustion 2006年8月
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102.
Three-Dimensional Numerical Simulation of Single Spinning and Two-Headed Detonations in a Circular Tube
The Problems of Modern Mechanics 2006年
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103.
Evaluation of ablation and longitudinal vortices in solid rocket motor by computational fluid dynamics
Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference 2006年
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104.
Effect of Boundary Layer for Wedge-Induced Attached Oblique Detonations
20th International Colloquium on the Dynamics of Explosions and Reactive Systems 2005年7月
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105.
Detailed Features of One-Dimensional Unsteady H2-Air Detonations
30th International Symposium on Combustion, Chicago 2004年7月
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106.
Longitudinal Oscillation Mode of One-Dimensional H2-Air Detonations
42nd AIAA Aerospace Sciences Meeting and Exhibit 2004年1月5日 American Institute of Aeronautics and Astronautics
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107.
Analogy between Wedge-induced Oblique Detonation and One-dimensional Piston-supported Detonation
19th International Colloquium on the Dynamics of Explosions and Reactive Systems 2003年7月
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108.
Heat Flux Estimation on the Nozzle Wall of Solid Rocket Motor Nozzle
23rd International Symposium on Space Technology and Science 2002年5月
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109.
The Reignition Process of One-Dimensional Detonations at Low Degree of Overdrive
28th International Symposium on Combustion, Edinburgh 2000年7月
知財情報はまだありません。
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