LASER VELOCIMETER AND HOT-WIRE ANEMOMETER COMPARISON IN A SUPERSONIC BOUNDARY-LAYER

被引:43
作者
JOHNSON, DA [1 ]
ROSE, WC [1 ]
机构
[1] NASA,AMES RES CTR,MOFFET FIELD,CA 94035
关键词
D O I
10.2514/3.49739
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:512 / 515
页数:4
相关论文
共 10 条
[1]  
Favre A, 1964, MECHANIQUE TURBULENC, P367
[2]   TURBULENCE MEASUREMENTS IN A MACH 2.9 BOUNDARY-LAYER USING LASER VELOCIMETRY [J].
JOHNSON, DA .
AIAA JOURNAL, 1974, 12 (05) :711-714
[3]   FLUCTUATION MEASUREMENTS IN A SUPERSONIC TURBULENT BOUNDARY LAYER [J].
KISTLER, AL .
PHYSICS OF FLUIDS, 1959, 2 (03) :290-296
[4]  
KLEBANOFF PS, 1955, NACA1247 REP
[5]  
MORKOVIN MV, 1958, AFOSRTN58469 JOHNS H
[6]   SHOCK WAVE TURBULENT BOUNDARY-LAYER INTERACTIONS IN RECTANGULAR CHANNELS [J].
REDA, DC ;
MURPHY, JD .
AIAA JOURNAL, 1973, 11 (02) :139-140
[7]  
ROSE WC, 1972, THESIS U WASHINGTON
[8]  
SANDBORN VA, 1974, TMX62337 NASA
[9]  
TIELEMAN HW, 1967, THESIS COLORADO STAT
[10]  
ZORIC DL, 1968, THESIS COLORADO STAT