AERODYNAMIC LOSS PENALTY PRODUCED BY FILM COOLING TRANSONIC TURBINE-BLADES

被引:31
作者
HALLER, BR [1 ]
CAMUS, JJ [1 ]
机构
[1] UNIV CAMBRIDGE,WHITTLE LAB,CAMBRIDGE,ENGLAND
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 1984年 / 106卷 / 01期
关键词
D O I
10.1115/1.3239535
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
引用
收藏
页码:198 / 205
页数:8
相关论文
共 14 条
[1]  
AMECKE J, 1970, VDI540 FORSCH, P16
[2]  
DENTON JD, ARC RM3775
[3]  
FOREST AE, 1982, COMMUNICATION APR
[4]  
FOREST AE, 1977, AGARDCP224 PAP
[5]   EFFECTS OF HOLE GEOMETRY AND DENSITY ON 3-DIMENSIONAL FILM COOLING [J].
GOLDSTEIN, RJ ;
ECKERT, ERG ;
BURGGRAF, F .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1974, 17 (05) :595-607
[6]  
GOSTELOW JP, ASME76GT62 PAP
[7]  
GREEN JE, RAE72231 TECHN REP
[8]  
HALLER BR, 1980, THESIS U CAMBRIDGE
[9]  
HARTSEL JE, AIAA7211 PAP
[10]  
HOADLEY D, CEGB RMN632 REP