Scaling of the streamwise velocity component in turbulent pipe flow

被引:176
作者
Morrison, JF [1 ]
McKeon, BJ
Jiang, W
Smits, AJ
机构
[1] Univ London Imperial Coll Sci & Technol, Dept Aeronaut, London SW7 2AZ, England
[2] Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA
[3] CARDC, Sichuan 621000, Peoples R China
关键词
D O I
10.1017/S0022112004008985
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Statistics of the streamwise velocity component in fully developed pipe flow are examined for Reynolds numbers in the range 5.5 x 10(4) less than or equal to Re-D less than or equal to 5.7 x 10(6). Probability density functions and their moments (up to sixth order) are presented and their scaling with Reynolds number is assessed. The second moment exhibits two maxima: the one in the viscous sublayer is Reynolds-number dependent while the other, near the lower edge of the log region, follows approximately the peak in Reynolds shear stress. Its locus has an approximate (R+)(0.5) dependence. This peak shows no sign of 'saturation', increasing indefinitely with Reynolds number. Scalings of the moments with wall friction velocity and (U-cl - (U) over bar) are examined and the latter is shown to be a better velocity scale for the outer region, y/R > 0.35, but in two distinct Reynolds-number ranges, one when Re-D < 6 x 10(4), the other when Re-D > 7 x 10(4). Probability density functions do not show any universal behaviour, their higher moments showing small variations with distance from the wall outside the viscous sublayer. They are most nearly Gaussian in the overlap region. Their departures from Gaussian are assessed by examining the behaviour of the higher moments as functions of the lower ones. Spectra and the second moment are compared with empirical and theoretical scaling laws and some anomalies are apparent. In particular, even at the highest Reynolds number, the spectrum does not show a self-similar range of wavenumbers in which the spectral density is proportional to the inverse streamwise wavenumber. Thus such a range does not attract any special significance and does not involve a universal constant.
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页码:99 / 131
页数:33
相关论文
共 72 条
[51]  
Nieuwstadt F. T. M., 1997, BOUNDARY LAYER SEPAR
[52]   Origin of the "-1" spectral law in wall-bounded turbulence [J].
Nikora, V .
PHYSICAL REVIEW LETTERS, 1999, 83 (04) :734-736
[53]   SCALING LAWS FOR PIPE-FLOW TURBULENCE [J].
PERRY, AE ;
ABELL, CJ .
JOURNAL OF FLUID MECHANICS, 1975, 67 (JAN28) :257-271
[54]   A WALL-WAKE MODEL FOR THE TURBULENCE STRUCTURE OF BOUNDARY-LAYERS .1. EXTENSION OF THE ATTACHED EDDY HYPOTHESIS [J].
PERRY, AE ;
MARUSIC, I .
JOURNAL OF FLUID MECHANICS, 1995, 298 :361-388
[55]   EXPERIMENTAL SUPPORT FOR THE ATTACHED-EDDY HYPOTHESIS IN ZERO-PRESSURE-GRADIENT TURBULENT BOUNDARY-LAYERS [J].
PERRY, AE ;
LI, JD .
JOURNAL OF FLUID MECHANICS, 1990, 218 :405-438
[56]   A THEORETICAL AND EXPERIMENTAL-STUDY OF WALL TURBULENCE [J].
PERRY, AE ;
HENBEST, S ;
CHONG, MS .
JOURNAL OF FLUID MECHANICS, 1986, 165 :163-199
[57]   ASYMPTOTIC SIMILARITY OF TURBULENCE STRUCTURES IN SMOOTH-WALLED AND ROUGH-WALLED PIPES [J].
PERRY, AE ;
ABELL, CJ .
JOURNAL OF FLUID MECHANICS, 1977, 79 (MAR23) :785-799
[58]  
Rotta JC, 1962, Prog Aero Sci, V2, P1, DOI DOI 10.1016/0376-0421(62)90014-3
[59]  
SANDBORN VA, 1955, 3266 NACA
[60]   AMPLITUDE-DEPENDENT NEUTRAL-MODES IN THE HAGEN-POISEUILLE FLOW THROUGH A CIRCULAR PIPE [J].
SMITH, FT ;
BODONYI, RJ .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 1982, 384 (1787) :463-489