High-altitude flight cooling investigation of a radial air-cooled engine
Description:
"An investigation of the cooling of an 18-cylinder, twin-row, radial, air-cooled engine in a high-performance pursuit airplane has been conducted for variable engine and flight conditions at altitudes ranging from 5000 to 35,000 feet in order to provide a basis for predicting high-altitude cooling performance from sea-level or low altitude experimental results. The engine cooling data obtained were analyzed by the usual NACA cooling-correlation method wherein cylinder-head and cylinder-barrel t…
more
Date:
May 9, 1946
Creator:
Manganiello, Eugene J.; Valerino, Michael F. & Bell, E. Barton
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department