The flow field behind surface mounted detached square ribs under the approaching flat plate turbulent boundary layer has been experimentally studied using the particle image velocimetry (PIV) (two-component and stereo) technique in both streamwise and cross stream measurement planes. An oil film visualization study has been carried out for correlating the surface flow patterns to the flow structures. The Reynolds number based on the rib height is equal to 11,075. The ratio of the gap height to the square rib size is set equal to 0.2, 0.37, 0.57, and 1.0. The ratio of approaching boundary layer thickness to rib height is equal to 0.2. The mean and rms velocity fields, streamwise and spanwise vorticity fields, velocity gradient and velocity vector fields, turbulent kinetic energy budgets, and stream trace results are reported. The second invariant of the velocity gradient tensor results are presented to distinguish between the rotational and shear contribution of the vorticity field. The recirculation bubbles with a focilike structure are observed behind the detached ribs. These structures are displaced upward, i.e., away from the wall surface with an increase in gap size of the detached cylinder. The size of the recirculation bubble also drops with an increase in the gap size. The stream traces in the cross stream plane show node-saddle patterns, whose near wall concentration is high for a lower gap size detached cylinder. The oil film visualization images show saddle patterns at the meeting point between the flow through the gap and the reattaching shear layer for the lower gap size detached cylinder. The v-velocity magnitude distribution shows greater wall-normal motion across the wake for the detached cylinder of lower gap size. There is a significant near wall velocity fluctuation for the lower gap size detached cylinder. The higher velocity fluctuation due to the near wall flow structures contributes toward an increase in the near wall mixing of a detached cylinder geometry. Overall, the present study clearly demonstrates the flow structures behind detached ribs, which are responsible for effective near wall mixing. The results from this study provide useful understanding for the design of turbulators in various practical applications.

1.
Taniguchi
,
S.
, and
Miyakoshi
,
K.
, 1990, “
Fluctuating Fluid Forces Acting on a Circular Cylinder and Interference With a Plane Wall, Effects of Boundary Layer Thickness
,”
Exp. Fluids
0723-4864,
9
, pp.
197
204
.
2.
Durao
,
D. F. G.
,
Gouveiu
,
P. S. T.
, and
Fereira
,
J. C. F.
, 1991, “
Velocity Characteristics of the Flow Around a Square Cross Section Cylinder Placed Near a Channel Wall
,”
Exp. Fluids
0723-4864,
11
, pp.
341
350
.
3.
Buresti
,
G.
, and
Lanciotti
,
A.
, 1992, “
Mean and Fluctuating Forces on a Circular Cylinder in Cross-Flow Near a Plane Surface
,”
J. Wind. Eng. Ind. Aerodyn.
0167-6105,
41–44
, pp.
639
650
.
4.
Liou
,
T. M.
, and
Wang
,
W. B.
, 1995, “
Laser Holographic Interferometry Study of Developing Heat Transfer in a Duct With a Detached Rib Array
,”
Int. J. Heat Mass Transfer
0017-9310,
38
, pp.
91
100
.
5.
Bosch
,
G.
,
Kappler
,
M.
, and
Rodi
,
W.
, 1996, “
Experiments on the Flow Past a Square Cylinder Placed Near a Wall
,”
Exp. Therm. Fluid Sci.
0894-1777,
13
, pp.
292
305
.
6.
Bailey
,
S. C. C.
,
Martinuzzi
,
R. J.
, and
Kopp
,
G. A.
, 2002, “
The Effects of Wall Proximity on Vortex Shedding From a Square Cylinder: Three Dimensional Effects
,”
Phys. Fluids
1070-6631,
14
, pp.
4160
4177
.
7.
Liou
,
T. M.
,
Chen
,
M. Y.
, and
Chang
,
K.
, 2003, “
Spectrum Analysis of Fluid Flow in a Rotating Two-Pass Duct With Detached 90° Ribs
,”
Exp. Therm. Fluid Sci.
0894-1777,
27
, pp.
313
321
.
8.
Liou
,
T. M.
,
Chen
,
M. Y.
, and
Wang
,
Y. M.
, 2003, “
Heat Transfer, Fluid Flow and Pressure Measurements Inside a Rotating Two-Pass Duct With Detached 90-deg Ribs
,”
ASME J. Turbomach.
0889-504X,
125
, pp.
565
574
.
9.
Martinuzzi
,
R. J.
,
Bailey
,
S. C. C.
, and
Kopp
,
G. A.
, 2003, “
Influence of Wall Proximity on Vortex Shedding From Square Cylinder
,”
Exp. Fluids
0723-4864,
34
, pp.
585
596
.
10.
Panigrahi
,
P. K.
,
Schroeder
,
A.
, and
Kompenhans
,
J.
, 2005, “
PIV Investigation of Flow Behind Surface Mounted Permeable Ribs
,”
Exp. Fluids
0723-4864,
40
, pp.
277
300
.
11.
Kolar
,
V.
, 1991, “
On the Critical Points in the Description of Vortical Flows
,”
Acta Mech.
0001-5970,
89
, pp.
241
245
.
12.
Zhou
,
Y.
, and
Antonia
,
R. A.
, 1994, “
Critical Points in a Turbulent Near Wake
,”
J. Fluid Mech.
0022-1120,
275
, pp.
59
81
.
13.
Brown
,
G. L.
, and
Roshko
,
A.
, 1974, “
On Density Effects and Large Structure in Turbulent Mixing Layers
,”
J. Fluid Mech.
0022-1120,
64
, pp.
775
816
.
14.
Jeong
,
J.
, and
Hussain
,
F.
, 1995, “
On the Identification of a Vortex
,”
J. Fluid Mech.
0022-1120,
285
, pp.
69
94
.
15.
Calluaud
,
D.
, and
David
,
L.
, 2004, “
Stereoscopic Particle Velocimetry Measurements of the Flow Around a Surface Mounted Block
,”
Exp. Fluids
0723-4864,
36
, pp.
53
61
.
16.
Wang
,
L.
,
Hejcik
,
J.
, and
Sunden
,
B.
, 2007, “
PIV Measurement of Separated Flow in a Square Channel With Streamwise Periodic Ribs on One Wall
,”
ASME J. Fluids Eng.
0098-2202,
129
, pp.
834
841
.
17.
Panigrahi
,
P. K.
,
Schroeder
,
A.
, and
Kompenhans
,
J.
, 2008, “
Turbulent Structures and Budgets Behind Permeable Ribs
,”
Exp. Therm. Fluid Sci.
0894-1777,
32
, pp.
1011
1033
.
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