FILM-COOLING EFFECTIVENESS AND SKIN FRICTION IN HYPERSONIC TURBULENT-FLOW

被引:48
作者
CARY, AM
HEFNER, JN
机构
关键词
D O I
10.2514/3.50348
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:1188 / +
页数:1
相关论文
共 16 条
[1]  
BECKWITH IE, 1971, D6221 NASA TN
[2]  
BERTRAM MH, 1968, HYPERSONIC BOUNDARY
[3]   ACTIVE COOLING HEAT PROTECTION [J].
BRUNNER, MJ .
JOURNAL OF SPACECRAFT AND ROCKETS, 1969, 6 (06) :661-&
[4]  
Cary A.M., 1970, AIAA J, V8, P2090, DOI [10.2514/3.6062, DOI 10.2514/3.6062]
[5]  
CHIN JH, 1958, NOV ASME ANN M NEW Y
[6]  
Goldberg T.J., 1971, TND6280 NASA
[7]  
GOLDSTEIN RJ, 1965, HTL60 U MINN MECH EN
[8]  
HARTNETT JP, 1960, AUG ASMEAICHE HEAT T
[9]  
LAGANELLI AL, 1970, AIAA70153 PAP
[10]  
MCCONARTY WA, 1968, 7305901001 BELL AER