Faculty - KANDA Takeshi |

（Last updated : 2024-11-20 16:50:56）

KANDA Takeshi

Department / Course College of Science and Engineering Department of Astronautics and Aeronautics

College of Engineering Department of Astronautics and Aeronautics

Graduate School of Engineering Department of Astronautics and Aeronautics

Job Professor

Academic background
	Tokyo University
～1984	The University of Tokyo
～1984	Aerospace Engineering Graduate School, Division of Engineering The University of Tokyo
～1982	The Faculty of Engineering The University of Tokyo

Business career
2017 ～	Professor Chubu University College of Engineering
1984 ～ 2003	Research Engineer

Belonging society
	American Institute of Aeronautics and Astronautics
	Japan Society for Aeronautical and Space Sciences
	The American Society of Mechanical Engineers

Present specialized field
Aerospace engineering keyword(High frequency combustion instability,detonation,laminar-turbulent transition,Fluid dynamics,Rocket,Scramjet,Ramjet,Ejector-jet,Aerospace plane,Combined-cycle)

Research, Studies
laminar-turbulent transition in pipe flow

Book and thesis
Books	"Combined-Cycle Engines," Encyclopedia of Aerospace Engineering 2010
Papers	Analytical study of rotating detonation and engine operating conditions Physics of Fluids 36,pp.116113 (Co-authored) 2024/11
Papers	Study of the reverse transition in pipe flow Scientific Reports 13,pp.12333 2023/07
Papers	Experimental study on high-frequency combustion instability of liquid-propellant rocket engines using off-design combustion model Acta Astonautica 202,pp.595-608 2022/02
Papers	Analytical Study on Detonation Pressure and Velocity Deficit Physics of Fluids 2022
Display All（231）

Research topic, funded research, and department laboratory expense
	Rocket-based combined-cycle engine

External Researcher ID
ORCID ID
0000-0002-5803-0558