Effect of Several Factors on the Cooling of a Radial Engine in Flight
Description:
"Flight tests of a Grumman Scout (XSF-2) airplane fitted with a Pratt & Whitney 1535 supercharged engine were conducted to determine the effect of engine power, mass flow of the cooling air, and atmospheric temperature on cylinder temperature. The tests indicated that the difference in temperature between the cylinder wall and the cooling air varied as the 0.38 power of the brake horsepower for a constant mass flow of cooling air, cooling-air temperature, engine speed, and brake fuel consumptio…
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Date:
November 1936
Creator:
Schey, Oscar W. & Pinkel, Benjamin
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department