Effects of compressibility on the performance of two full-scale helicopter rotors /
Paul J. Carpenter.

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Main Author: Carpenter, Paul J.
Related Names: United States. National Advisory Committee for Aeronautics.
Language(s): English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Subjects: Pitching (Aerodynamics)
Rotors (Helicopters) > Rotors (Helicopters) / Testing.
Summary: An investigation has been conducted on the Langley helicopter test tower to determine experimentally the effects of compressibility on the performance and blade pitching moments of two full-scale helicopter rotors with twisted and untwisted blades over a tip-speed range from 350 to 770 feet per second.
Note: NACA TN No. 2277.
"January 1951."
Physical Description: 17 p. : ill. ; 28 cm.
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