Flight investigation to determine aerodynamic characteristics of propeller at forward Mach numbers up to about 0.95; efficiency is approximately 79% at Mach number of 0.948 and advance ratio of 3.5.
Effect of advance ratio on flight performance of modified supersonic propeller
NACA -- Tech Note
NACA -- Technical Note ; n 4389
1958
20 pages
Article (Journal)
English
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