REYNOLDS-NUMBER EFFECT ON THE SKIN FRICTION IN SEPARATED FLOWS BEHIND A BACKWARD-FACING STEP

被引:86
作者
JOVIC, S
DRIVER, D
机构
[1] NASA,AMES RES CTR,MOFFETT FIELD,CA 94035
[2] ELORET INST,PALO ALTO,CA 94303
关键词
D O I
10.1007/BF00208471
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Results from the present study show that the skin-friction coefficient decreases as the Reynolds number, Reh, increases in the following manner, Cf,min=-0.19 Reh-1/2. The -1/2 power relationship deduced from the correlation Cf,min vs. Rehindicates laminar like behavior which is consistent with the findings of Adams et al. (1984). Clauser's method, which is frequently used for the determination of the wall shear stress, leads to erroneous results when applied to the velocity measurements obtained in the near field of reattaching flows (and many other wall-bounded nonequilibrium flows). Direct measurements of the Cfusing the LOI technique give higher values than those obtained by the classical techniques. The normalized mean velocity on the wall coordinates violates the universal law-of-the-wall in the near field of reattaching flows. © 1995 Springer-Verlag.
引用
收藏
页码:464 / 467
页数:4
相关论文
共 9 条
[1]  
Adams E. W., 1984, MD43 STANF U DEP MEC
[2]   THE STRUCTURE OF A TURBULENT SHEAR-LAYER BOUNDING A SEPARATION REGION [J].
CASTRO, IP ;
HAQUE, A .
JOURNAL OF FLUID MECHANICS, 1987, 179 :439-468
[3]  
DAVENPORT LW, 1991, AIAA J, V29, P25
[4]  
DEBREDOROD V, 1972, IC7219 AER REP
[5]   FEATURES OF A REATTACHING TURBULENT SHEAR-LAYER IN DIVERGENT CHANNEL FLOW [J].
DRIVER, DM ;
SEEGMILLER, HL .
AIAA JOURNAL, 1985, 23 (02) :163-171
[6]  
JOVIC S, 1994, NASA108807 TECHN MEM
[7]  
LE H, 1993, TF58 STANF U DEP MEC
[8]  
Monson D. J., 1981, ICIASF'81 Record. International Congress on Instrumentation in Aerospace Simulation Facilities, P232
[9]   SKIN FRICTION MEASUREMENTS BY A DUAL-LASER-BEAM INTERFEROMETER TECHNIQUE [J].
MONSON, DJ ;
HIGUCHI, H .
AIAA JOURNAL, 1981, 19 (06) :739-744