Rchr

J-GLOBAL ID：200901062526205883 Update date: Mar. 08, 2009

Chinzei Nobuo

チンゼイノブオ | Chinzei Nobuo

Affiliation and department：

Research field (1)： Aerospace engineering

Research keywords (3)：超音速燃焼 , 超音速流 , スクラムジェット

Research theme for competitive and other funds (2)：

宇宙推進、超音速燃焼ラムジェット(スクラムジェット)、超音速流
宇宙推進

MISC (6)：

Spreading of Two-Stream Supersonic Turbulent Mixing Layer. Physics of Fluids, Vol.29, No.5, pp.1345-1347 (1986)
Prediction of Pre-Combustion Shock in Scramjet Combustors-A New Method. Proc. 18th ISTS, pp.183-188 (1992)
Effects of Injector Geometry on Scramjet Combustor Performance. Journal of Propulsion and Power Vol.9, No.1, pp.146-152 (1993)
Spreading of Two-Stream Supersonic Turbulent Mixing Layer. Physics of Fluids, Vol.29, No.5, pp.1345-1347 (1986)
Prediction of Pre-Combustion Shock in Scramjet Combustors-A New Method. Proc. 18th ISTS, pp.183-188 (1992)

ｍore...

Education (2)：

- 1968 Tokyo Institute of Technology School of Engineering
Tokyo Institute of Technology

Professional career (1)：

Doctor of Engineering

Association Membership(s) (2)：

Japan Society of Mechanical Engineers , Japan Society for Aeronautical and Space Sciences

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