AERODYNAMIC LOSS IN A GAS-TURBINE STAGE WITH FILM COOLING

被引:41
作者
ITO, S [1 ]
ECKERT, ERG [1 ]
GOLDSTEIN, RJ [1 ]
机构
[1] UNIV MINNESOTA,DEPT MECH ENGN,MINNEAPOLIS,MN 55455
来源
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME | 1980年 / 102卷 / 04期
关键词
D O I
10.1115/1.3230368
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
引用
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页码:964 / 970
页数:7
相关论文
共 8 条
[1]  
HARTSEL JE, 1972, ASME7211 PAP
[2]  
ITO S, 1976, THESIS U MINNESOTA
[3]  
ITO S, 1978, ASME, V100, P476
[4]   The approxiamte integration of the differential equation of laminar boundary layer [J].
Pohlhausen, K .
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1921, 1 :252-268
[5]  
PRUST HW, 1972, AIAA7212 PAP
[6]  
SHAPIRO AH, 1947, ASME J APPLIED MECHA, pA317
[7]  
TABAKOFF W, 1975, AIAA75843 PAP
[8]  
TABAKOFF W, 1972, ASME72GT46 PAP