The effect of fill volume on the heat transfer performance of a hybrid cooling fin thermosyphon, characterized by an airfoil cross-sectional shape and a slot-shaped cavity, is investigated. The performance was examined at three fill volumes, expressed as a percentage of the evaporator section: 0%, 60%, and 240%. These were chosen to represent three distinct regimes: unfilled, filled, and overfilled evaporator sections, respectively. The cross section of this copper–water thermosyphon has a NACA0010 shape with a chord length of 63.5 mm and an aspect ratio (ratio of the length of the evaporator section to the cavity width) of 1.109. The evaporator length comprises 8.3% of the total thermosyphon length. The air-cooled condenser section was placed in a uniform air flow in the test section of an open return wind tunnel. The rate of heat transfer, or performance, was measured as a function of fill volume and evaporator temperature. The heat transfer performance increased by 100–170% by adding 0.86 ml of working fluid (de-ionized water), i.e., when the fill volume increased from 0% to 60%, which illustrates the improvement of a cooling fin's heat transfer rate by converting it to a hybrid cooling fin thermosyphon. Of the fill volumes investigated, the thermosyphon achieves a maximum heat transfer rate and highest average surface temperature at the 60% fill volume. Overfilling the evaporator section at 240% fill results in a slight decrease in performance from the 60% fill volume. The results of this study demonstrate the feasibility of hybridizing a cooling fin to act both as a cooling fin and a thermosyphon.
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Experimental Investigation of the Heat Transfer Performance of a Hybrid Cooling Fin Thermosyphon
Christina A. Pappas,
Christina A. Pappas
1
Department of Mechanical and Aerospace Engineering,
Charlottesville, VA 22904
e-mail: caj5p@virginia.edu
University of Virginia
,122 Engineer's Way
,Charlottesville, VA 22904
e-mail: caj5p@virginia.edu
1Corresponding author.
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Donald A. Jordan,
Donald A. Jordan
Senior Research Scientist
Department of Mechanical and Aerospace Engineering,
Charlottesville, VA 22904
e-mail: dj8n@virginia.edu
Department of Mechanical and Aerospace Engineering,
University of Virginia
,122 Engineer's Way
,Charlottesville, VA 22904
e-mail: dj8n@virginia.edu
Search for other works by this author on:
Pamela M. Norris
Pamela M. Norris
Professor
Fellow ASME
Department of Mechanical and Aerospace Engineering,
Charlottesville, VA 22904
e-mail: pamela@virginia.edu
Fellow ASME
Department of Mechanical and Aerospace Engineering,
University of Virginia
,122 Engineer's Way
,Charlottesville, VA 22904
e-mail: pamela@virginia.edu
Search for other works by this author on:
Christina A. Pappas
Department of Mechanical and Aerospace Engineering,
Charlottesville, VA 22904
e-mail: caj5p@virginia.edu
University of Virginia
,122 Engineer's Way
,Charlottesville, VA 22904
e-mail: caj5p@virginia.edu
Donald A. Jordan
Senior Research Scientist
Department of Mechanical and Aerospace Engineering,
Charlottesville, VA 22904
e-mail: dj8n@virginia.edu
Department of Mechanical and Aerospace Engineering,
University of Virginia
,122 Engineer's Way
,Charlottesville, VA 22904
e-mail: dj8n@virginia.edu
Pamela M. Norris
Professor
Fellow ASME
Department of Mechanical and Aerospace Engineering,
Charlottesville, VA 22904
e-mail: pamela@virginia.edu
Fellow ASME
Department of Mechanical and Aerospace Engineering,
University of Virginia
,122 Engineer's Way
,Charlottesville, VA 22904
e-mail: pamela@virginia.edu
1Corresponding author.
Contributed by the Heat Transfer Division of ASME for publication in the JOURNAL OF HEAT TRANSFER. Manuscript received August 5, 2013; final manuscript received July 2, 2014; published online July 29, 2014. Assoc. Editor: Patrick E. Phelan.
J. Heat Transfer. Oct 2014, 136(10): 104502 (5 pages)
Published Online: July 29, 2014
Article history
Received:
August 5, 2013
Revision Received:
July 2, 2014
Citation
Pappas, C. A., Jordan, D. A., and Norris, P. M. (July 29, 2014). "Experimental Investigation of the Heat Transfer Performance of a Hybrid Cooling Fin Thermosyphon." ASME. J. Heat Transfer. October 2014; 136(10): 104502. https://doi.org/10.1115/1.4028000
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