Report on cooling system tests of DH-4 airplane equipped with experimental auxiliary radiator in the propeller slipstream
United States. Army. Air Service. Engineering Division.
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DescriptionOne object of these tests was to determine on the required additional radiating surface (for the DH-4 airplane), placed in the propeller slipstream, to insure satisfactory cooling at any given air temperature. Another object was to determine the relative cooling value of a square foot of surface in a nose position and in the slipstream of the propeller about one-half its diameter back.
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