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Experiments on the Recovery of Waste Heat in Cooling Ducts, Special ReportTests have been conducted in the N.A.C.A. full-scale wind tunnel to investigate the partial recovery of the heat energy which is apparently wasted in the cooling of aircraft engines. The results indicate that if the radiator is located in an expanded duct, a part of the energy lost in cooling is recovered; however, the energy recovery is not of practical importance up to airplane speeds of 400 miles per hour. Throttling of the duct flow occurs with heated radiators and must be considered in designing the duct outlets from data obtained with cold radiators in the ducts.
Document ID
20090015245
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Silverstein, Abe
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 1939
Subject Category
Aeronautics (General)
Report/Patent Number
NACA-SR-111
Report Number: NACA-SR-111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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