Determination of Installed Reciprocating Engine Cooling Requirements Through Flight Test
830718
02/01/1983
- Event
- 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.
- 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.