中部大学

中部大学

教員情報

苅田 丈士 KANDA Takeshi

プロフィール

職名 教授
所属 工学部 宇宙航空理工学科
工学部 機械工学科
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)
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
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
研究紹介PDF
授業科目 熱力学、工業力学、航空宇宙工学
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

"Expander and Coolant Bleed Cycles of Methane-Fueled Rocket Engine," to be published, Tran. JSASS.

"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.

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