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KANDA Takeshi



Title Professor
Belong to Dept. of Astronautics and Aeronautics
Dept. of Mechanical Engineering
Mechanical Engineering (graduate school)
Graduated Master of Engineering, Tokyo University
Degree Doctor of Engineering, Tokyo University
Academic Institutional Membership Japan Society for Aeronautical and Space Sciences (JSASS)
American Institute of Aeronautics and Astronautics (AIAA)
Field of Study Propulsion, Fluid Dynamics, Thermal Engineering
Research, Studies Liquid Rocket Engine, Jet Engine, Space Transportation, Turbulent Transition, Pseudo-Shock Wave
Curriculum Specialized Thermodynamics, Fluid dynamics, Rocket Engineering, Jet Engine
Contact Mail

Books Published, Translation

"Combined-Cycle Engines," Encyclopedia of Aerospace Engineering, Vol.2.,John Wiley & Sons Ltd

Academic Papers, Critique

"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," Tran. 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, 2003, pp.859-867.

Lectures, Symposium, Presentation

"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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