THE INFLUENCE OF A LAMINAR BOUNDARY-LAYER AND LAMINAR INJECTION ON FILM COOLING PERFORMANCE

被引:22
作者
GOLDSTEIN, RJ [1 ]
YOSHIDA, T [1 ]
机构
[1] NATL AEROSP LAB,TOKYO,JAPAN
来源
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME | 1982年 / 104卷 / 02期
关键词
D O I
10.1115/1.3245096
中图分类号
O414.1 [热力学];
学科分类号
摘要
引用
收藏
页码:355 / 362
页数:8
相关论文
共 25 条
[1]  
BERGELES G, 1976, THESIS U LONDON
[2]  
CRAWFORD ME, 1980, NASA CR3219
[3]  
ERIKSEN VL, 1971, NASA CR72991
[4]  
GOLDSTEIN RJ, 1970, ISRAEL J TECHNOL, V8, P145
[5]  
GOLDSTEIN RJ, 1968, NASA CR54604
[6]   LEADING-EDGE INJECTION FOR FILM COOLING OF TURBINE VANES [J].
HANUS, GJ ;
ECUYER, MRL .
JOURNAL OF ENERGY, 1977, 1 (01) :44-49
[7]  
HARTNETT JP, 1956, HTL TR10 U MINN
[8]  
HIROKI T, 1974, ASME74GT30 PAP
[9]   NATURE OF JETS ENTERING A TURBULENT-FLOW .B. FILM COOLING PERFORMANCE [J].
KADOTANI, K ;
GOLDSTEIN, RJ .
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1979, 101 (03) :466-470
[10]  
LAUFER J, 1954, NACA TR1174