TURBULENCE MEASUREMENTS IN A COMPRESSIBLE BOUNDARY-LAYER

被引:9
作者
ROSE, WC [1 ]
机构
[1] NASA,AMES RES CTR,MOFFETT FIELD,CA 94035
关键词
D O I
10.2514/3.49411
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:1060 / 1064
页数:5
相关论文
共 13 条
[1]   BOUNDARY-LAYER PITOT AND HOT-WIRE SURVEYS AT M INFINITY APPROXIMATELY EQUAL TO 20 [J].
FISCHER, MC ;
MADDALON, DV ;
WEINSTEI.LM ;
WAGNER, RD .
AIAA JOURNAL, 1971, 9 (05) :826-&
[2]  
GRANDE E, 1971, THESIS U WASHINGTON
[3]  
KEMP WH, 1972, D6965 NASA TN
[4]   FLUCTUATION MEASUREMENTS IN A SUPERSONIC TURBULENT BOUNDARY LAYER [J].
KISTLER, AL .
PHYSICS OF FLUIDS, 1959, 2 (03) :290-296
[5]   TURBULENCE IN SUPERSONIC FLOW [J].
KOVASZNAY, LSG .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (10) :657-&
[6]   THE HOT-WIRE ANEMOMETER IN SUPERSONIC FLOW [J].
KOVASZNAY, LSG .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (09) :565-&
[7]  
LADERMAN AJ, 1972, AIAA7273 PAP
[8]  
MORKOVIN MV, AD158279
[9]  
MORKOVIN MV, 1958, TN58469 J HOPK U AFO
[10]  
MORKOVIN MV, 1955, 1955 P HEAT TRANSF F