Air-Cooling Effects of Fins on a Motorcycle Engine : 1st Report, Influence of Running Speed and Fin-Pitch

2002 ◽  
Vol 2002 (0) ◽  
pp. 9-10
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Masago YAMAMOTO
2004 ◽  
Vol 2004.3 (0) ◽  
pp. 183-184
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Kohei NAKASHIMA ◽  
Masago YAMAMOTO

2006 ◽  
Vol 49 (3) ◽  
pp. 869-875 ◽  
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Kohei NAKASHIMA ◽  
Masago YAMAMOTO

2005 ◽  
Vol 71 (709) ◽  
pp. 2324-2330 ◽  
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Kohei NAKASHIMA ◽  
Masago YAMAMOTO

2003 ◽  
Vol 2003.78 (0) ◽  
pp. _13-13_-_13-14_
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Masago YAMAMOTO

2003 ◽  
Vol 2003.3 (0) ◽  
pp. 151-152
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Masago YAMAMOTO

2004 ◽  
Vol 2004 (0) ◽  
pp. 103-104
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Kohei NAKASHIMA ◽  
Masago YAMAMOTO

2004 ◽  
Vol 2004.57 (0) ◽  
pp. 141-142
Author(s):  
Masao YOSHIDA ◽  
Soichi ISHIHARA ◽  
Yoshio MURAKAMI ◽  
Kohei NAKASHIMA ◽  
Masao YAMAMOTO

2006 ◽  
Author(s):  
Zakirhusen K. Memon ◽  
T. Sundararajan ◽  
V. Lakshminarasimhan ◽  
Y. R. Babu ◽  
Vinay Harne

Author(s):  
Tsuyoshi Hiroki ◽  
Ichiro Katsumata

Several problem areas associated with air-cooling of small turbine blades and vanes are identified. These problem areas include the leading edge cooling by film and impingement cooling, comparison of several configurations for trailing edge cooling, effects of Mach number on blade surface heat transfer, effects of film cooling on the aerodynamic performances of turbine cascades, the method of data correlation for the application of heat transfer data taken with low temperature, low pressure rig tests to high temperature, high pressure conditions. Experimental data are presented for each discussed area. The description of design and experimental data of one of the experimental cooled blades and vanes are presented.


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