Flow structure due to dimple depressions on a channel surface

被引:236
作者
Ligrani, PM [1 ]
Harrison, JL [1 ]
Mahmmod, GI [1 ]
Hill, ML [1 ]
机构
[1] Univ Utah, Dept Mech Engn, Convect Heat Transfer Lab, Salt Lake City, UT 84112 USA
关键词
D O I
10.1063/1.1404139
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Instantaneous, dynamic and time-averaged characteristics of the vortex structures which are shed from the dimples placed on one wall of a channel are described. The dimpled test surface contains 13 staggered rows of dimples in the streamwise direction, where each dimple has a print diameter of 5.08 cm, and a ratio of depth to print diameter of 0.2. Considered are Reynolds numbers (based on channel height) Re-H from 600 to 11 000, and ratios of channel height to dimple print diameter H/D of 0.25, 0.50, and 1.00. For all three H/D, a primary vortex pair is periodically shed from the central portion of each dimple, including a large upwash region. This shedding occurs periodically and continuously, and is followed by inflow advection into the dimple cavity. The frequency of these events appears to scale on time-averaged bulk velocity and dimple print diameter, which gives nondimensional frequencies of 2.2-3.0 for all three H/D values considered. As H/D decreases, (i) the strength of the primary vortex pair increases, and (ii) two additional secondary vortex pairs (which form near the spanwise edges of each dimple) become significantly stronger, larger in cross section, and more apparent in flow visualization images and in surveys of time-averaged, streamwise vorticity. The locations of these primary and secondary vortex pairs near the dimpled surface coincide closely with locations where normalized Reynolds normal stress is augmented. This evidences an important connection between the vortices, Reynolds normal stress, and mixing. The large-scale unsteadiness associated with this mixing is then more pronounced, and encompasses larger portions of the vortex structure (and thus extends over larger volumes) as H/D increases from 0.25 to 1.0. (C) 2001 American Institute of Physics.
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页码:3442 / 3451
页数:10
相关论文
共 11 条
[1]   CONTROL OF CIRCULAR-CYLINDER FLOW BY THE USE OF DIMPLES [J].
BEARMAN, PW ;
HARVEY, JK .
AIAA JOURNAL, 1993, 31 (10) :1753-1756
[2]   GOLF BALL AERODYNAMICS [J].
BEARMAN, PW ;
HARVEY, JK .
AERONAUTICAL QUARTERLY, 1976, 27 (MAY) :112-122
[3]  
Gromov P. R., 1986, Soviet Technical Physics Letters, V12, P547
[4]   FLUID DYNAMIC EFFECTS OF GROOVES ON CIRCULAR-CYLINDER SURFACE [J].
KIMURA, T ;
TSUTAHARA, M .
AIAA JOURNAL, 1991, 29 (12) :2062-2068
[5]   Flow visualization and flow tracking as applied to turbine components in gas turbine engines [J].
Ligrani, P .
MEASUREMENT SCIENCE AND TECHNOLOGY, 2000, 11 (07) :992-1006
[6]  
LIGRANI PM, 1989, EXP FLUIDS, V7, P424
[7]   MINIATURE 5-HOLE PRESSURE PROBE FOR MEASUREMENT OF 3 MEAN VELOCITY COMPONENTS IN LOW-SPEED FLOWS [J].
LIGRANI, PM ;
SINGER, BA ;
BAUN, LR .
JOURNAL OF PHYSICS E-SCIENTIFIC INSTRUMENTS, 1989, 22 (10) :868-876
[8]   DESCRIBING THE UNCERTAINTIES IN EXPERIMENTAL RESULTS [J].
MOFFAT, RJ .
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 1988, 1 (01) :3-17
[9]  
Shchukin A. B., 1998, Applied Energy: Russian Journal of Fuel, Power and Heat Systems, V36, P45
[10]  
TEREKHOV VI, 1995, RUSS J ENG THERMOPHY, V5, P11