苅田 丈士 KANDA Takeshi
プロフィール
| 職名 | 教授 |
|---|---|
| 所属 |
理工学部 宇宙航空学科 工学部 宇宙航空理工学科 大学院 工学研究科 宇宙航空理工学専攻 大学院 工学研究科 機械工学専攻 |
| 最終学歴 | 東京大学大学院工学系研究科航空学専攻修士課程修了 |
| 学位 | 博士（工学）（東京大学） |
| 資格 | 高圧ガス製造保安責任者、火薬類取扱保安責任者、第3種電気主任技術者 |
| 所属学会・役職 | 日本航空宇宙学会 アメリカ航空宇宙学会 |
| 専門分野 | エンジン工学、流体力学 |
| 研究テーマ | 液体ロケットエンジン、ジェットエンジン、宇宙輸送、乱流遷移、衝撃波
|
| 授業科目 | 熱力学、流体力学、ロケット工学、ジェットエンジン |
| 公開連絡先 | メールアドレス：kanda-t@isc.chubu.ac.jp |
著書および訳書
"Combined-Cycle Engines," Encyclopedia of Aerospace Engineering, Vol.2.,John Wiley & Sons Ltd
学術論文、評論
"Off-Design Combustion in Liquid-Propellant Rocket Engine with High-Frequency Instability," Tran. JSASS, Vol.62, No.6, 2019, pp.331-333.
"Expander and Coolant Bleed Cycles of Methane-Fueled Rocket Engine," Trans. JSASS, Vol.61, No.3, 2018, pp.106-118.
"Conservation-Law Approach on Transition in a Pipe Flow," Tran. JSASS, Vol.59, No.6, 2016, pp.356-363.
"Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines," Tran. JSASS, Vol.59, No.6, 2016, pp.332-339.
"Extended Tsiolkovskii Equation and its Application to Launch Vehicles," J. Spacecraft & Rockets, Vol.53, No.5, 2016, pp.969-979.
"Experimental Study of Heat Flux in the Pseudo-shock Region," Tran. JSASS, Vol.59, No.5, 2016, pp.305-309.
"Conceptual Design Model of High-Altitude Test Stand for Rocket Engines," Tran. JSASS, Vol.59, No.3, 2016, pp.161-169.
"Analytical Method for Prediction of Suction Performance of Ejector-Jet," Tran. JSASS, Vol.58, No.4, 2015, pp.228-236.
"Conceptual Study of Throttled Operation of Rocket Engine Turbopump," Tran. JSASS, Vol.56, No.1, 2013, pp.49-60.
"Conservation-Law Approach to Prediction of Length of Boundary Layer Transition Region," Tran. JSASS, Vol.55, No.5, 2012, pp.295－303.
"Prediction of Pseudo-Shock Position in a Long Duct Using Momentum Balance Model," Tran. JSASS, Vol.55, No. 3, 2012, pp.199-201.
"Conservation-Law Approach to Prediction of Boundary Layer Transition," Tran. JSASS, Vol.54, No.183, 2011, pp.7-15.
"Experimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet Mode," J. Propulsion and Power, Vol.23, No.6, 2007, pp.1153-1159.
"Mach 8 Tests of a Combined-Cycle Engine Combustor," J. Propulsion and Power, Vol.23, No.5, 2007, pp.1018-1022.
"Conceptnal Study of a Rocket-Ramjet Combined-Cycle Engine for an Aero space Plane," J. Propulsion and Power, Vol.23, No.2, 2007, pp.301-309.
"Conceptual Study of a Combined Cycle Engine for an Aerospace Plane," J. Propulsion and Power, Vol.19, No.5, pp.2003, 859-867.
講演、シンポジウム、学会発表
"Design of Sub-Scale Rocket-Ramjet Combined Cycle Engine Model," 56th IAC, 2005.
"Momentum Balance Model of Flow Field with Pseudo-shock," AIAA 43rd Aerospace Sciences Meeting, 2005.
"Transient Analysis of LOX/LH２ Rocket Engine (LE-7)," AIAA 25th Joint Propulsion Conf., 1989.
