Flight Measurements of Section Efficiency, Thrust, and Power of a Supersonic-Type Propeller at Mach Numbers to 0.9
Description: Report discussing testing on a supersonic-type propeller designed for a forward Mach number of 0.95, advance ratio of 2.2, and power coefficient of 0.26. Thrust distributions were found to be smooth and uniform over a range of Mach numbers, indicating efficient operation.
Date: January 11, 1956
Creator: Hammack, Jerome B. & O'Bryan, Thomas C.
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Partner: UNT Libraries Government Documents Department