Determination of Installed Reciprocating Engine Cooling Requirements Through Flight Test

830718

02/01/1983

Event
Business Aircraft Meeting and Exposition
Authors Abstract
Content
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 air-cooled 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.
Meta TagsDetails
DOI
https://doi.org/10.4271/830718
Pages
12
Citation
Miley, S., Ward, D., and Kelley, M., "Determination of Installed Reciprocating Engine Cooling Requirements Through Flight Test," SAE Technical Paper 830718, 1983, https://doi.org/10.4271/830718.
Additional Details
Publisher
Published
Feb 1, 1983
Product Code
830718
Content Type
Technical Paper
Language
English