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Experiments with a built-in or fuselage radiatorThe experiments discussed here were performed to determine whether radiators having similar cooling properties offer less resistance when incorporated into the fuselage, than when the hitherto customary arrangement is employed, with the radiator in the free air current more or less independent of the fuselage. The experiments indicated that the quantity of air flowing through the radiator is greatest when the fuselage and the radiator are separate. However, separate radiators cause more air resistance. When the radiator is incorporated into the fuselage, it is only possible to obtain a quantity equal to that which flows through the radiator in the free air current if the lateral outlet vents are widened or the quantity of air in increased by some special means, such as fans. Whether it is possible, in practice, to obtain the necessary cooling effect in this way, together with reduced resistance of the fuselage, is not decided here, since it is a question of construction.
Document ID
19930081039
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wiesselsberger, C
(Gottingen Aerodynamic Laboratory)
Date Acquired
September 6, 2013
Publication Date
May 1, 1923
Report/Patent Number
NACA-TN-141
Report Number: NACA-TN-141
Accession Number
93R10329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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