Experimental results, measured on and above a dimpled test surface placed on one wall of a channel, are given for Reynolds numbers from 1250 to 61,500 and ratios of air inlet stagnation temperature to surface temperature ranging from 0.68 to 0.94. These include flow visualizations, surveys of time-averaged total pressure and streamwise velocity, and spatially resolved local Nusselt numbers, which are measured using infrared thermography, used in conjunction with energy balances, thermocouples, and in situ calibration procedures. The ratio of channel height to dimple print diameter is 0.5. Flow visualizations show vortical fluid and vortex pairs shed from the dimples, including a large upwash region and packets of fluid emanating from the central regions of each dimple, as well as vortex pairs and vortical fluid that form near dimple diagonals. These vortex structures augment local Nusselt numbers near the downstream rims of each dimple, both slightly within each depression, and especially on the flat surface just downstream of each dimple. Such augmentations are spread over larger surface areas and become more pronounced as the ratio of inlet stagnation temperature to local surface temperature decreases. As a result, local and spatially averaged heat transfer augmentations become larger as this temperature ratio decreases. This is due to the actions of vortical fluid in advecting cool fluid from the central parts of the channel to regions close to the hotter dimpled surface.
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January 2001
Technical Papers
Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel
G. I. Mahmood, Graduate Student,
G. I. Mahmood, Graduate Student
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
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M. L. Hill, Graduate Student,
M. L. Hill, Graduate Student
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
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D. L. Nelson, Graduate Student,
D. L. Nelson, Graduate Student
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
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P. M. Ligrani, Professor.,
P. M. Ligrani, Professor.
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
11
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H.-K. Moon, Consulting Engineer,
H.-K. Moon, Consulting Engineer
Solar Turbines, Inc., Turbine Cooling Design and Analysis, San Diego, CA 92186
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B. Glezer, Head, Turbine Cooling and Heat Transfer Analysis
B. Glezer, Head, Turbine Cooling and Heat Transfer Analysis
Solar Turbines, Inc., Turbine Cooling Design and Analysis, San Diego, CA 92186
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G. I. Mahmood, Graduate Student
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
M. L. Hill, Graduate Student
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
D. L. Nelson, Graduate Student
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
P. M. Ligrani, Professor.
11
Convective Heat Transfer Laboratory, Department of Mechanical Engineering, University of Utah, Salt Lake City, UT 84112
H.-K. Moon, Consulting Engineer
Solar Turbines, Inc., Turbine Cooling Design and Analysis, San Diego, CA 92186
B. Glezer, Head, Turbine Cooling and Heat Transfer Analysis
Solar Turbines, Inc., Turbine Cooling Design and Analysis, San Diego, CA 92186
Contributed by the International Gas Turbine Institute and presented at the 45th International Gas Turbine and Aeroengine Congress and Exhibition, Munich, Germany, May 8–11, 2000. Manuscript received by the International Gas Turbine Institute February 2000. Paper No. 2000-GT-230. Review Chair: D. Ballal.
J. Turbomach. Jan 2001, 123(1): 115-123 (9 pages)
Published Online: February 1, 2000
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Received:
February 1, 2000
Citation
Mahmood, G. I., Hill, M. L., Nelson, D. L., Ligrani, P. M., Moon, H., and Glezer, B. (February 1, 2000). "Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel ." ASME. J. Turbomach. January 2001; 123(1): 115–123. https://doi.org/10.1115/1.1333694
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