FILM COOLING ON A GAS-TURBINE ROTOR BLADE

被引：117
|
作者：
TAKEISHI, K [1 ]
AOKI, S [1 ]
SATO, T [1 ]
TSUKAGOSHI, K [1 ]
机构：
[1] MITSUBISHI HEAVY IND CO LTD, TAKASAGO MACHINERY WORKS, TAKASAGO, JAPAN
来源：
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1992年 / 114卷 / 04期
关键词：
D O I：
10.1115/1.2928036
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The film cooling effectiveness on a low-speed stationary cascade and the rotating blade has been measured by using a heat-mass transfer analogy. The film cooling effectiveness on the suction surface of the rotating blade fits well with that on the stationary blade, but a low level of effectiveness appears on the pressure surface of the rotating blade. In this paper, typical film cooling data will be presented and film cooling on a rotating blade is discussed.
引用
收藏
页码：828 / 834
页数：7
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