The thermal performance of a miniature, three-dimensional flat-plate oscillating heat pipe (3D FP-OHP) was experimentally investigated during high-gravity loading with nonfavorable evaporator positioning. The heat pipe had dimensions of 3.0 × 3.0 × 0.254 cm3 and utilized a novel design concept incorporating a two-layer channel arrangement. The device was charged with acetone and tested at a heat input of 95 W within a spin-table centrifuge. It was found that the heat pipe operated and performed near-independent of the investigated hypergravity loading up to 10 g. Results show that at ten times the acceleration due to gravity (10 g), the effective thermal conductivity was almost constant and even slightly increased which is very different from a conventional heat pipe. The gravity-independent heat transfer performance provides a unique feature of OHPs.
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Robust Thermal Performance of a Flat-Plate Oscillating Heat Pipe During High-Gravity Loading
S. M. Thompson,
S. M. Thompson
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
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A. A. Hathaway,
A. A. Hathaway
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
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C. D. Smoot,
C. D. Smoot
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
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C. A. Wilson,
C. A. Wilson
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
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H. B. Ma,
H. B. Ma
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
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R. M. Young,
R. M. Young
Northrop Grumman Corporation
, Linthicum, MD 21090
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L. Greenberg,
L. Greenberg
Northrop Grumman Corporation
, Linthicum, MD 21090
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B. R. Osick,
B. R. Osick
Northrop Grumman Corporation
, Linthicum, MD 21090
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S. Van Campen,
S. Van Campen
Northrop Grumman Corporation
, Linthicum, MD 21090
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B. C. Morgan,
B. C. Morgan
U.S. Army Research Laboratory
, Adelphi, MD 20783
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D. Sharar,
D. Sharar
U.S. Army Research Laboratory
, Adelphi, MD 20783
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N. Jankowski
N. Jankowski
U.S. Army Research Laboratory
, Adelphi, MD 20783
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S. M. Thompson
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
A. A. Hathaway
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
C. D. Smoot
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
C. A. Wilson
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
H. B. Ma
Department of Mechanical & Aerospace Engineering,
University of Missouri
, Columbia, MO 65211
R. M. Young
Northrop Grumman Corporation
, Linthicum, MD 21090
L. Greenberg
Northrop Grumman Corporation
, Linthicum, MD 21090
B. R. Osick
Northrop Grumman Corporation
, Linthicum, MD 21090
S. Van Campen
Northrop Grumman Corporation
, Linthicum, MD 21090
B. C. Morgan
U.S. Army Research Laboratory
, Adelphi, MD 20783
D. Sharar
U.S. Army Research Laboratory
, Adelphi, MD 20783
N. Jankowski
U.S. Army Research Laboratory
, Adelphi, MD 20783J. Heat Transfer. Oct 2011, 133(10): 104504 (5 pages)
Published Online: August 19, 2011
Article history
Received:
January 20, 2011
Accepted:
April 13, 2011
Online:
August 19, 2011
Published:
August 19, 2011
Citation
Thompson, S. M., Hathaway, A. A., Smoot, C. D., Wilson, C. A., Ma, H. B., Young, R. M., Greenberg, L., Osick, B. R., Campen, S. V., Morgan, B. C., Sharar, D., and Jankowski, N. (August 19, 2011). "Robust Thermal Performance of a Flat-Plate Oscillating Heat Pipe During High-Gravity Loading." ASME. J. Heat Transfer. October 2011; 133(10): 104504. https://doi.org/10.1115/1.4004076
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