An experimental and numerical study was conducted to determine the thermal performance of V-shaped ribs in a rectangular channel with an aspect ratio of 2:1. Local heat transfer coefficients were measured using the steady state thermochromic liquid crystal technique. Periodic pressure losses were obtained with pressure taps along the smooth channel sidewall. Reynolds numbers from 95,000 to 500,000 were investigated with V-shaped ribs located on one side or on both sides of the test channel. The rib height-to-hydraulic diameter ratios (eDh) were 0.0625 and 0.02, and the rib pitch-to-height ratio (Pe) was 10. In addition, all test cases were investigated numerically. The commercial software FLUENT™ was used with a two-layer k-ε turbulence model. Numerically and experimentally obtained data were compared. It was determined that the heat transfer enhancement based on the heat transfer of a smooth wall levels off for Reynolds numbers over 200,000. The introduction of a second ribbed sidewall slightly increased the heat transfer enhancement whereas the pressure penalty was approximately doubled. Diminishing the rib height at high Reynolds numbers had the disadvantage of a slightly decreased heat transfer enhancement, but benefits in a significantly reduced pressure loss. At high Reynolds numbers small-scale ribs in a one-sided ribbed channel were shown to have the best thermal performance.

1.
Sattelmayer
,
T.
, and
Polifke
,
W.
, 1998, “
NOx-Abatement Potential of Lean-Premixed GT-Combustors
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
120
, pp.
48
59
.
2.
Kim
,
W. K.
,
Arellano
,
L.
,
Vardakas
,
M.
,
Moon
,
H.
, and
Smith
,
K.
, 2003, “
Comparison of Trip-Strip/Impingement/Dimple Cooling Concepts at High Reynolds Numbers
,” ASME Paper No. GT2003-38935.
3.
Bailey
,
J. C.
,
Tolpadi
,
A. K.
,
Intile
,
J.
,
Fric
,
T. F.
,
Nirmalan
,
N. V.
, and
Bunker
,
R. S.
, 2002, “
Experimental and Numerical Study of Heat Transfer in a Gas Turbine Combustor Liner
,” ASME Paper No. GT2002-30183.
4.
Ligrani
,
P. M.
,
Oliveira
,
M. M.
, and
Blaskovich
,
T.
, 2003, “
Comparison of Heat Transfer Augmentation Techniques
,”
AIAA J.
0001-1452,
41
, pp.
337
362
.
5.
Cakan
,
M.
, 2000, “
Aero-Thermal Performance of Internal Cooling Systems in Turbo Machines
,”
Lecture Series 2000–03
,
von Karman Institute for Fluid Dynamics
.
6.
Lau
,
S. C.
,
Kukreja
,
R. T.
, and
McMillan
,
R. D.
, 1991, “
Effects of V-Shaped Rib Arrays on Turbulent Heat Transfer and Friction of Fully Developed Flow in a Square Channel
,”
Int. J. Heat Mass Transfer
0017-9310,
34
, pp.
1605
1616
.
7.
Han
,
J. C.
,
Zhang
,
Y. M.
, and
Lee
,
C. P.
, 1991, “
Augmented Heat Transfer in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs
,”
ASME J. Heat Transfer
0022-1481,
113
, pp.
590
596
.
8.
Taslim
,
M. E.
,
Li
,
T.
, and
Kercher
,
D. M.
, 1996, “
Experimental Heat Transfer and Friction in Channels Roughened With Angled, V-Shaped, and Discrete Ribs on Two Opposite Walls
,”
ASME J. Turbomach.
0889-504X,
118
, pp.
20
28
.
9.
Al-Hadhrami
,
L.
,
Griffith
,
T.
, and
Han
,
J. C.
, 2003, “
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=2) With Five Different Orientations of 45deg V-Shaped Rib Turbulators
,”
ASME J. Heat Transfer
0022-1481,
125
, pp.
232
242
.
10.
Cho
,
H. H.
,
Rhee
,
D. H.
, and
Lee
,
D. H.
, 2002, “
Effects of Duct Aspect Ratio on Heat/Mass Transfer With Discrete V-Shaped Ribs
,” ASME Paper No. GT2002-38622.
11.
Wright
,
L. M.
,
Fu
,
W. L.
, and
Han
,
J. C.
, 2004, “
Thermal Performance of Angled, V-Shaped, and W-Shaped Rib Turbulators in Rotating Rectangular Cooling Channels (AR=4:1)
,” ASME Paper No. GT2004-54073.
12.
Su
,
G.
,
Teng
,
S.
,
Chen
,
H. C.
, and
Han
,
J. C.
, 2003, “
Computation of Flow and Heat Transfer in Rotating Rectangular Channels (AR=4) With V-Shaped Ribs by a Reynolds Stress Turbulence Model
,” ASME Paper No. GT2003-38348.
13.
Gao
,
X.
, and
Sundén
,
B.
, 2001, “
Heat Transfer Distribution in Rectangular Ducts With V-Shaped Ribs
,”
Heat Mass Transfer
0947-7411,
37
, pp.
315
320
.
14.
Lee
,
E.
,
Wright
,
L. M.
, and
Han
,
J. C.
, 2003, “
Heat Transfer in Rotating Rectangular Channels (AR=4:1) With V-Shaped and Angled Rib Turbulators With and Without Gaps
,” ASME Paper No. GT2003-38900.
15.
Momin
,
A. E.
,
Saine
,
J. S.
, and
Solanki
,
S. C.
, 2002, “
Heat Transfer and Friction in Solar Air Heater Duct With V-Shaped Rib Roughness on an Absorber Plate
,”
Int. J. Heat Mass Transfer
0017-9310,
45
, pp.
3383
3396
.
16.
Ireland
,
P. T.
, and
Jones
,
T. C.
, 2000, “
Liquid Crystal Measurements of Heat Transfer and Surface Shear Stress
,”
Meas. Sci. Technol.
0957-0233,
11
, pp.
969
986
.
17.
Hanjalić
,
K.
, and
Launder
,
B. E.
, 1972, “
Fully Developed Asymmetric Flow in a Plane Channel
,”
J. Fluid Mech.
0022-1120,
51
, pp.
301
335
.
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