An investigation was conducted in the N.A.C.A. 20-foot wind tunnel to determine the drag, the propulsive and net efficiencies, and the cooling characteristics of severa1 scale-model arrangements of air-cooled radial-engine nacelles and present-day propellers in front of an 18- percent-thick, 5- by 15-foot airfoil. This report deals with an investigation of wing-nacelle arrangements simulating the geometric proportions of airplanes in the 40,000- to 70,000- pound weight classification and having the nacelles located in the vicinity of the optimum location determined from the earlier tests.
Tests of Several Model Nacelle-Propeller Arrangements in Front of a Wing
1939-09-01
Sonstige
Keine Angabe
Englisch
Tests of wing-nacelle-propeller combination at several pitch settings up to 42°
Engineering Index Backfile | 1936
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