A flight test procedure has been developed which will provide a systematic means of working cooling installation problems for air-cooled reciprocating engine aircraft. The procedure is based upon the NACA Cooling Correlation analysis which resulted from the radial aircooled engine development program over forty years ago. The derivation of the method and results from flight test programs to prove the method are reported in this paper.
Determination of installed reciprocating engine cooling requirements through flight test
Bestimmung des Kuehlbedarfs eines installierten Motors durch Flugversuch
SAE-Papers ; 1-9
1983
9 Seiten, 14 Bilder, 25 Quellen
Conference paper
English
Determination of Installed Reciprocating Engine Cooling Requirements Through Flight Test
SAE Technical Papers | 1983
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