HOT-WIRE INVESTIGATION OF AN UNSEPARATED SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTION

被引:13
作者
HAYAKAWA, K
SMITS, AJ
BOGDONOFF, SM
机构
关键词
D O I
10.2514/3.48490
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:579 / 585
页数:7
相关论文
共 22 条
[1]  
ARDONCEAU P, 1979, NATO AGARD CP271
[2]   EFFECT OF MEAN COMPRESSION OR DILATATION ON TURBULENCE STRUCTURE OF SUPERSONIC BOUNDARY-LAYERS [J].
BRADSHAW, P .
JOURNAL OF FLUID MECHANICS, 1974, 63 (APR29) :449-464
[3]  
BRADSHAW P, 1973, AGARDOGRAPH 169
[4]  
HANCOCK P. E., 1980, THESIS U LONDON
[5]  
HAYAKAWA K, 1983, MAE1600 PRINC U REPT
[6]  
HAYAKAWA K, 1983, P S STRUCTURE COMPLE, P279
[7]  
KLEBANOFF PS, 1955, NACA TR1247
[8]   THE HOT-WIRE ANEMOMETER IN SUPERSONIC FLOW [J].
KOVASZNAY, LSG .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (09) :565-&
[9]   INVESTIGATION OF A 3-DIMENSIONAL SHOCK-WAVE SEPARATED TURBULENT BOUNDARY-LAYER [J].
KUSSOY, MI ;
VIEGAS, JR ;
HORSTMAN, CC .
AIAA JOURNAL, 1980, 18 (12) :1477-1484
[10]  
LEE DH, 1979, THESIS U POITIERS