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Convective Array Cooling for a Solar Powered AircraftA general characteristic of photovoltaics is that they increase in efficiency as their operating temperature decreases. Based on this principal, the ability to increase a solar aircraft's performance by cooling the solar cells was examined. The solar cells were cooled by channeling some air underneath the cells and providing a convective cooling path to the back side of the array. A full energy balance and flow analysis of the air within the cooling passage was performed. The analysis was first performed on a preliminary level to estimate the benefits of the cooling passage. This analysis established a clear benefit to the cooling passage. Based on these results a more detailed analysis was performed. From this cell temperatures were calculated and array output power throughout a day period were determined with and without the cooling passage. The results showed that if the flow through the cooling passage remained laminar then the benefit in increased output power more than offset the drag induced by the cooling passage.
Document ID
20030015690
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Colozza, Anthony J.
(Analex Corp. Brook Park, OH United States)
Dolce, James
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-13737
NAS 1.26:212084
NASA/CR-2003-212084
Funding Number(s)
PROJECT: RTOP 708-87-11
CONTRACT_GRANT: NAS3-00145
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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