The present study deals with the numerical prediction of turbulent flow and heat transfer in a 2:1 aspect ratio rectangular duct with ribs on the two shorter sides. The ribs are of square cross section, staggered and aligned normal (90 deg) to the main flow direction. The ratio of rib height to duct hydraulic diameter equals 0.063, and the ratio of rib spacing to rib height equals 10. The duct may be stationary or rotating. The axis of rotation is normal to the axis of the duct and parallel to the ribbed walls (i.e., the ribbed walls form the leading and the trailing faces). The problem is three dimensional and fully elliptic; hence, for computational economy, the present analysis deals only with a periodically fully developed situation where the calculation domain is limited to the region between two adjacent ribs. Turbulence is modeled with the k–ε model in conjunction with wall functions. However, since the rib height is small, use of wall functions necessitates that the Reynolds number be kept high. (Attempts to use a two-layer model that permits integration to the wall did not yield satisfactory results and such modeling issues are discussed at length.) Computations are made here for Reynolds number in the range 30,000–100,000 and for Rotation number = 0 (stationary), 0.06, and 0.12. For the stationary case, the predicted heat transfer agrees well with the experimental correlations. Due to the Coriolis-induced secondary flow, rotation is found to enhance heat transfer from the trailing and the side walls, while decreasing heat transfer from the leading face. Relative to the corresponding stationary case, the effect of rotation is found to be less for a ribbed channel as compared to a smooth channel.

1.
Prakash
C.
, and
Zerkle
R.
, “
Prediction of Turbulent Flow and Heat Transfer in a Radially Rotating Square Duct
,”
ASME JOURNAL OF TURBOMACHINERY
, Vol.
114
,
1992
, pp.
835
846
.
2.
Launder
B. E.
, and
Spalding
D. B.
, “
The Numerical Computation of Turbulent Flows
,”
Computer Methods in Applied Mechanics and Engineering
, Vol.
3
,
1974
, pp.
269
289
.
3.
Patel
V. C.
,
Rodi
W.
, and
Scheuerer
G.
, “
Turbulence Models for Near-Wall and Low-Reynolds Number Flows: A Review
,”
AIAA Journal
, Vol.
23
, No.
9
,
1985
, pp.
1308
1319
.
4.
Rodi, W., “Experience With Two-Layer Models Combining the k–ε Model With a One-Equation Model Near the Wall,” Paper No. AIAA-91-0216, 1991.
5.
Webb
R. L.
,
Eckert
E. R. G.
, and
Goldstein
R. J.
, “
Heat Transfer and Friction in Tubes With Repeated-Rib Roughness
,”
Int. J. Heat Mass Transfer
, Vol.
14
,
1971
, pp.
601
617
.
6.
Chang
B. H.
, and
Mills
A. F.
, “
Application of a Low-Reynolds Number Turbulence Model to Flow in a Tube With Repeated Rectangular Rib Roughness
,”
PHOENICS Journal
, Vol.
4
, No.
3
,
1991
, pp.
262
288
.
7.
Arman
B.
, and
Rabas
T.
, “
The Influence of the Prandtl Number on the Thermal Performance of Tubes With the Separation and Reattachment Mechanism
,”
Enhanced Heat Transfer
, ASME HTD-Vol.
202
,
1992
, pp.
77
88
.
8.
Cunha, F. J., “Turbulent Flow and Heat Transfer in Gas Turbine Blade Cooling Passages,” ASME 92-GT-239, 1992.
9.
Burgraff, F., “Experimental Heat Transfer and Pressure Drop With Two Dimensional Turbulence Promoters Applied to Two Opposite Walls of a Square Tube,” Augmentation of Convective Heat and Mass Transfer, E. E. Bergles and R. L. Webb, eds., ASME, New York, 1970, pp. 70–79.
10.
Han
J. C.
,
Glicksman
L. R.
, and
Rohsenow
W. M.
, “
An Investigation of Heat Transfer and Friction for Rib-Roughened Surfaces
,”
Int. J. Heat Mass Transfer
, Vol.
21
,
1978
, pp.
1143
1156
.
11.
Han
J. C.
, “
Heat Transfer and Friction Characteristics in Rectangular Channels With Rib Turbulators
,”
ASME Journal of Heat Transfer
, Vol.
110
,
1988
, pp.
321
328
.
12.
Han
J. C.
, and
Park
J. S.
, and
Lei
C. K.
, “
Augmented Heat Transfer in Rectangular Channels of Narrow Aspect Ratios With Rib Turbulators
,”
Int. J. Heat Mass Transfer
, Vol.
32
, No.
9
,
1989
, pp.
1619
1630
.
13.
Taslim, M. E., and Spring, S. D., “Experimental Heat Transfer and Friction Factors in Turbulated Cooling Passages of Different Aspect Ratios Where Turbulators Are Staggered,” Paper No. AIAA-88-3014, 1988.
14.
Wagner, J. H., Kim, J. C., and Johnson, B. V., “Rotating Heat Transfer Experiments With Turbine Airfoil Internal Flow Passages,” ASME 86-GT-133, 1986.
15.
Johnson
B. V.
,
Wagner
J. H.
,
Steuber
G. D.
, and
Yeh
F. C.
, “
Heat Transfer in Rotating Serpentine Passages With Trips Skewed to the Flow
,”
ASME JOURNAL OF TURBOMACHINERY
, Vol.
116
,
1994
, pp.
113
123
.
16.
Taslim
M. E.
,
Bondi
L. A.
, and
Kercher
D. M.
, “
An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened With 45 deg Criss-Cross Ribs on Two Opposite Walls
,”
ASME JOURNAL OF TURBOMACHINERY
, Vol.
113
,
1991
, pp.
345
353
.
17.
Taslim
M. E.
,
Rahman
A.
, and
Spring
S. D.
, “
An Experimental Investigation of Heat Transfer Coefficients in a Spanwise Rotating Channel With Two Opposite Rib-Roughened Walls
,”
ASME JOURNAL OF TURBOMACHINERY
, Vol.
113
,
1991
, pp.
75
82
.
18.
Patankar
S. V.
,
Liu
C. H.
, and
Sparrow
E. M.
, “
Fully Developed Flow and Heat Transfer in Ducts Having Streamwise-Periodic Variations of Cross-Sectional Area
,”
ASME Journal of Heat Transfer
, Vol.
99
,
1977
, pp.
180
186
.
19.
Rosten
H. I.
, and
Worrell
J. K.
, “
Generalized Wall Functions for Turbulent Flow
,”
PHOENICS Journal
, Vol.
1
,
1988
, pp.
81
109
.
20.
Jayatillika
C. L. V.
, “
The Influence of the Prandtl Number and Surface Roughness on the Resistance of the Sub-layer to Momentum and Heat Transfer
,”
Prog. in Heat and Mass Transfer
, Vol.
1
,
1969
, pp.
193
329
.
21.
Iacovides
H.
, and
Launder
B. E.
, “
Parametric and Numerical Study of Fully Developed Flow and Heat Transfer in Rotating Rectangular Ducts
,”
ASME JOURNAL OF TURBOMACHINERY
, Vol.
113
,
1991
, pp.
331
338
.
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