A rod was positioned upstream of a circular cylinder to enhance its heat transfer in an air stream. The diameter of the cylinder was 40mm and the diameter of the rod ranged from 1to12mm. The distance between the axes of the cylinder and the rod was varied between 40 and 120mm and the Reynolds number ranged from 1.5×104 to 6.2×104. In the optimum configuration, the heat transfer on the front face of the cylinder increases remarkably relative to a single circular cylinder, and results in a 40% overall increase in heat transfer.

1.
Lesage
,
F.
, and
Gartshore
,
L. S.
, 1987, “
A Method of Reducing Drag and Fluctuating Side Force on Bluff Bodies
,”
J. Wind. Eng. Ind. Aerodyn.
0167-6105,
25
, pp.
229
245
.
2.
Tsutsui
,
T.
, and
Igarashi
,
T.
, 2002, “
Drag Reduction of a Circular Cylinder in an Air-Stream
,”
J. Wind. Eng. Ind. Aerodyn.
0167-6105,
90
, pp.
527
541
.
3.
Igarashi
,
T.
, 1997, “
Drag Reduction of a Square Prism by Flow Control Using a Small Rod
,”
J. Wind. Eng. Ind. Aerodyn.
0167-6105,
69–71
, pp.
141
153
.
4.
Zhang
,
P. F.
,
Wang
,
J. J.
,
Lu
,
S. F.
, and
Mi
,
J.
, 2005, “
Aerodynamic Characteristics of a Square Cylinder With a Rod in a Staggered Arrangement
,”
Exp. Fluids
0723-4864,
35-4
, pp.
494
502
.
5.
Sarioglu
,
M.
,
Akansu
,
Y. E.
, and
Yavuz
,
T.
, 2005, “
Control of Around Square Cylinders at Incidence by Using a Rod
,”
AIAA J.
0001-1452,
43–7
, pp.
1419
1426
.
6.
Prasad
,
A.
, and
Williamson
,
C. H. K.
, 1997, “
A Method for the Reduction of Bluff Body Drag
,”
J. Wind. Eng. Ind. Aerodyn.
0167-6105,
69–71
, pp.
155
167
.
7.
Eckert
,
E. G. G.
, and
Drake
, Jr.,
R. M.
,
Heat and Mass Transfer
, 2nd ed.,
McGraw-Hill
,
New York
, p.
242
.
8.
Tsutsui
,
T.
,
Igarashi
,
T.
, and
Nakamura
,
H.
, 2001, “
Drag Reduction and Heat Transfer Enhancement of a Square Prism
,”
JSME Int. J., Ser. B
1340-8054,
44–4
, pp.
575
583
.
9.
Igarashi
,
T.
, and
Tsutsui
,
T.
, 1998, “
Enhancement of Heat Transfer and Reduction of Drag of a Square Prism Arranged Diamond-Shape in an Air Stream
,” in
Proceedings of the 11th IHTC
,
Kyongju
, Korea, Vol.
5
, pp.
261
266
.
10.
Perkins
, Jr.,
H. C.
, and
Leppert
,
G.
, 1964, “
Local Heat-Transfer Coefficients on a Uniformly Heated Cylinder
,”
Int. J. Heat Mass Transfer
0017-9310,
7
, pp.
143
158
.
11.
Chang
,
B. H.
, and
Mills
,
A. F.
, 2004, “
Effect of Aspect Ratio on Forced Convection Heat Transfer From Cylinders
,”
Int. J. Heat Mass Transfer
0017-9310,
47
, pp.
1289
1296
.
12.
Igarashi
,
T.
, and
Hirata
,
M.
, 1977, “
Heat Transfer in Separated Flows, Part 2: Theoretical Analysis
,”
Heat Transfer-Jpn. Res.
0096-0802,
6
(
3
), pp.
60
78
.
13.
Zukauskas
,
A.
, 1972, “
Heat Transfer From Tube in Crossflow
,”
Advances in Heat Transfer
,
Academic
,
New York
, Vol.
8
, pp.
93
160
.
14.
Kline
,
S. J.
, 1985, “
The Purposes of Uncertainty Analysis
,”
ASME J. Fluids Eng.
0098-2202,
107
, pp.
153
160
.
15.
Achenbach
,
E.
, 1968, “
Distribution of Local Pressure and Skin Friction Around a Circular Cylinder in Cross-Flow up to Re=5×106
,”
J. Fluid Mech.
0022-1120,
34
, part 4, pp.
625
639
.
16.
Bearman
,
P. W.
, 1969, “
On Vortex Shedding From a Circular Cylinder in the Critical Reynolds Number Regime
,”
J. Fluid Mech.
0022-1120,
37
, part 3, pp.
577
585
.
17.
Schlichting
,
H.
, 1968,
Boundary Layer Theory
, 6th ed.,
McGraw-Hill
,
New York
, p.
17
.
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