Heat transfer and friction coefficients measurements have been obtained for fully developed, turbulent internal flows in circular tubes with six different concavity (dimple) surface array geometries. Two different concavity depths and three different concavity array densities were tested using tube bulk flow Reynolds numbers from 20,000 to 90,000. Liquid-crystal thermography was used to measure the temperature distributions on the outside of the concavity tubes. Using the average heat transfer coefficient for the fully developed region, the overall heat transfer enhancements are compared to baseline smooth tube results. Friction coefficients are also compared to values for a smooth tube. Dimple depths of 0.2–0.4 relative to the dimple surface diameter were used, with surface area densities ranging from 0.3 to 0.7. Dimple arrays were all in-line geometries. The results showed that heat transfer enhancements for dimpled internal surfaces of circular passages can reach factors of 2 or more when the relative dimple depth is greater than 0.3 and the dimple array density is about 0.5 or higher. The associated friction factor multipliers for such configurations are in the range of 4–6. The present study provides a first insight into the heat transfer and friction effects of various concavity arrays for turbulent flows.

1.
Bearman
,
P. W.
, and
Harvey
,
J. K.
,
1976
, “
Golf Ball Aerodynamics
,”
Aeronaut. Q.
,
27
, May, pp.
112
122
.
2.
Bearman
,
P. W.
, and
Harvey
,
J. K.
,
1993
, “
Control of Circular Cylinder Flow by the Use of Dimples
,”
AIAA J.
,
31
(
10
), pp.
1753
1756
.
3.
Kiknadze, G. I., Gachechiladze, I. A., and Oleinikov, V. G., 2000, “Method and Apparatus for Controlling the Boundary or Wall Layer of a Continuous Medium,” US Patent No. 6,119,987.
4.
Lake, J. P., King, P. I., and Rivir, R. B., 2000, “Low Reynolds Number Loss Reduction on Turbine Blades with Dimples and V-Grooves,” AIAA Paper No. 00-0738, 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno.
5.
Khalatov, A. A., 2001, “Vortex Technologies in Aerospace Engineering,” Proceedings of the U.S.-Ukrainian Workshop on Innovative Combustion and Aerothermal Technologies in Energy and Power Systems, May 20–25, Kiev.
6.
Afanas’yev
,
V. N.
,
Veselkin
,
V. Yu.
,
Leont’ev
,
A. I.
,
Skibin
,
A. P.
, and
Chudnovskiy
,
Ya. P.
,
1993
, “
Thermohydraulics of Flow Over Isolated Depressions (Pits, Grooves) in a Smooth Wall
,”
Heat Transfer-Sov. Res.
,
25
(
1
), pp.
22
56
.
7.
Isaev
,
S. A.
,
Leont’ev
,
A. I.
, and
Baranov
,
P. A.
,
2000
, “
Identification of Self-Organized Vortexlike Structures in Numerically Simulated Turbulent Flow of a Viscous Incompressible Liquid Streaming around a Well on a Plane
,”
Tech. Phys. Lett.
,
26
(
1
), pp.
15
18
.
8.
Kesarev
,
V. S.
, and
Kozlov
,
A. P.
,
1993
, “
Convective Heat Transfer in Turbulized Flow Past a Hemispherical Cavity
,”
Heat Transfer-Sov. Res.
,
25
, pp.
156
160
.
9.
Schukin, A. V., Kozlov, A. P., and Agachev, R. S., 1995, “Study and Application for Hemispherical Cavities for Surface Heat Transfer Augmentation,” IGTI Turbo Expo, Paper No. 95-GT-59, Houston.
10.
Syred, N., Khalatov, A., Kozlov, A., Shchukin, A., and Agachev, R., 2000, “Effect of Surface Curvature on Heat Transfer and Hydrodynamics within a Single Hemispherical Dimple,” IGTI Turbo Expo, Paper No. 2000-GT-236, Munich.
11.
Afanas’yev
,
V. N.
, and
Chudnovskiy
,
Ya. P.
,
1992
, “
Heat Transfer and Friction on Surfaces Contoured by Spherical Depressions
,”
Heat Transfer-Sov. Res.
,
24
, pp.
24
104
.
12.
Afanas’yev
,
V. N.
,
Chudnovsky
,
Ya. P.
,
Leont’ev
,
A. I.
, and
Roganov
,
P. S.
,
1993
, “
Turbulent Flow Friction and Heat Transfer Characteristics for Spherical Cavities on a Flat Plate
,”
Exp. Therm. Fluid Sci.
,
7
, pp.
1
8
.
13.
Belen’kiy
,
M. Ya.
,
Gotovskii
,
M. A.
,
Lekakh
,
B. M.
,
Fokin
,
B. S.
, and
Khabenskii
,
V. B.
,
1992
, “
Experimental Study of the Thermal and Hydraulic Characteristics of Heat Transfer Surfaces Formed by Spherical Cavities
,”
Teplofiz. Vys. Temp.
,
29
(
6
), pp.
1142
1147
.
14.
Belen’kiy
,
M. Ya.
,
Gotovskii
,
M. A.
,
Lekakh
,
B. M.
,
Fokin
,
B. S.
, and
Dolgushin
,
K. S.
,
1993
, “
Heat Transfer Augmentation Using Surfaces Formed by a System of Spherical Cavities
,”
Heat Transfer-Sov. Res.
,
25
, pp.
196
202
.
15.
Chyu, M. K., Yu, Y., Ding, H., Downs, J. P., and Soechting, F. O., 1997, “Concavity Enhanced Heat Transfer in an Internal Cooling Passage,” IGTI Turbo Expo, Paper No. 97-GT-437, Orlando.
16.
Moon, H. K., O’Connell, T., and Glezer, B., 1999, “Channel Height Effect on Heat Transfer and Friction in a Dimpled Passage,” IGTI Turbo Expo, Paper No. 99-GT-163, Indianapolis.
17.
Mahmood, G. I., Hill, M. L., Nelson, D. L., Ligrani, P. M., Moon, H. K., and Glezer, B., 2000, “Local Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel,” IGTI Turbo Expo, Paper No. 2000-GT-230, Munich.
18.
Nagoga, G. P., 1996, “Effective Methods of Cooling of Blades of High Temperature Gas Turbines,” Publishing House of Moscow Aerospace Institute (in Russian), p. 100.
19.
Farina
,
D. J.
,
Hacker
,
J. M.
,
Moffat
,
R. J.
, and
Eaton
,
J. K.
,
1994
, “
Illuminant Invariant Calibration of Thermochromic Liquid Crystals
,”
Exp. Therm. Fluid Sci.
9
, pp.
1
9
.
20.
Boelter, L. M. K., Young, G., and Iversen, H. W., 1948, “An Investigation of Aircraft Heaters XXVII—Distribution of Heat Transfer Rate in the Entrance Region of a Tube,” NACA TN 1451.
21.
Dittus, F. W., and Boelter, L. M. K., 1930, University of California at Berkeley Publications in Engineering, Vol. 2, p. 443.
22.
Holman, J. P., 1976, Heat Transfer, McGraw-Hill Book Co., 4th edition, p. 204.
23.
Kline
,
S. J.
, and
McClintock
,
F. A.
,
1953
, “
Describing Uncertainties in Single-Sample Experiments
,” Mech. Eng. (Am. Soc. Mech. Eng.), Jan., pp. 3–8.
24.
Webb
,
R. L.
,
Eckert
,
E. R. G.
, and
Goldstein
,
R. J.
,
1971
, “
Heat Transfer and Friction in Tubes with Repeated Rib Roughness
,”
Int. J. Heat Mass Transfer
,
14
, pp.
601
617
.
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