Convective heat transfer with pin-fin arrays have been studied extensively in laboratory experiments where flow is introduced to the array uniformly over the channel span. However, the flow path in actual cooling designs is often serpentine-shaped with multiple turns, and the pin-fin array section is often located immediately downstream of a turn. The present study, using an analogous mass transfer technique based on naphthalene sublimation, investigates the effects of three different, nonaxial flow entries on array heat transfer for both an inline and a staggered arrangement of pins. The measurement acquires the mass transfer rate of each individual pin in a five row by seven column array for the Reynolds number varying from 8000 to 25,000. The mass transfer and associated flow visualization results indicate that the highly nonuniform flow distribution established at the array entrance and persisting through the entire array can have significant effects on the array heat transfer characteristics. Compared to the conventional case with axial-through flow entrance, the overall array heat transfer performance can be either enhanced or degraded, depending on the actual inlet arrangements and array configurations.

1.
Ambrose, D., Lawenson, I. J., and Sprake, C. H. S., 1975, “The Vapor Pressure of Naphthalene,” J. Chem, Thermo., pp. 1173–1176.
2.
Armstrong, J., and Winstanly, D., 1987, “A Review of Staggered Array Pin Fin Heat Transfer for Turbine Cooling Applications,” ASME Paper 87-GT-201.
3.
Brigham
B. A.
, and
VanFossen
G. J.
,
1984
, “
Length-to-Diameter Ratio and Row Number Effects in Short Pin Fin Heat Transfer
,”
ASME Journal of Engineering for Gas Turbines and Power
, Vol.
106
, pp.
241
246
.
4.
Chyu
M. K.
,
1990
, “
Heat Transfer and Pressure Drop for Short Pin-Fin Arrays With Pin-Endwall
,”
ASME JOURNAL OF HEAT TRANSFER
, Vol.
112
, pp.
926
932
.
5.
Chyu
M. K.
, and
Goldstein
R. J.
,
1991
, “
Influence of Cylindrical Elements on Local Mass Transfer from a Flat Surface
,”
Int. J. Heat and Mass Transfer
, Vol.
34
, pp.
2175
2186
.
6.
Chyu, M. K., Hsing, Y. C, Shih, T. I-P., and Natarajan, V., 1998, “Heat Transfer Contributions of Pins and Endwall in Pin-Fin Arrays: Effects of Thermal Boundary Condition Modeling,” ASME Paper 98-GT-175. ASME Journal of Turbomachinery, accepted for publication.
7.
Eckert, E. R. G., 1976, “Analogies to Heat Transfer Processes,” Measurements in Heat Transfer, E. R. G. Eckert and R. J. Goldstein, eds., Hemisphere, New York.
8.
Metzger
D. E.
,
Berry
R. A.
, and
Benson
J. P.
,
1982
a, “
Developing Heat Transfer in Rectangular Ducts With Staggered Arrays of Short Pin Fins
,”
ASME JOURNAL OF HEAT TRANSFER
, Vol.
104
, pp.
700
706
.
9.
Metzger, D. E., and Haley, S. W., 1982b, “Heat Transfer Experiments and Flow Visualization of Arrays of Short Pin Fins,” ASME Paper 82-GT-138.
10.
Metzger, D. E., Fan, Z. X., Shepard, W. B., 1982c, “Pressure Loss and Heat Transfer Through Multiple Rows of Short Pin Fins,” Heat Transfer 1982, Vol. 3, Hemisphere, New York, pp. 137–142.
11.
Metzger
D. E.
,
Fan
C. S.
, and
Haley
S. W.
,
1984
, “
Effects of Pin Shape and Array Orientation on Heat Transfer and Pressure Loss in Pin Fin Arrays
,”
ASME Journal of Engineering for Gas Turbines and Power
, Vol.
106
, pp.
252
257
.
12.
Metzger, D. E., and Shepard, W. B., 1986, “Row Resolved Heat Transfer Variations in Pin Fin Arrays Including Effects of Non-Uniform Arrays and Flow Convergence,” ASME Paper 86-GT-132.
13.
Simoneau
R. J.
, and
VanFossen
G. J.
,
1984
, “
Effect of Location in an Array on Heat Transfer to a Short Cylinder in Crossflow
,”
ASME JOURNAL OF HEAT TRANSFER
, Vol.
106
, pp.
42
48
.
14.
Sparrow
E. M.
, and
Ramsey
J. W.
,
1978
, “
Heat Transfer and Pressure Drop for a Staggered Wall-Attached Array of Cylinders with Tip Clearance
,”
Int. J. Heat Mass Transfer
, Vol.
21
, pp.
1369
1378
.
15.
VanFossen
G. J.
,
1982
, “
Heat Transfer Coefficient for Staggered Arrays of Short Pin Fins
,”
ASME Journal of Engineering for Gas Turbines and Power
, Vol.
104
, pp.
268
274
.
16.
Zukauskas
A. A.
,
1972
, “
Heat Transfer from Tubes in Cross Flow
,”
Advances in Heat Transfer
, Vol.
8
, pp.
116
133
.
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