Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98, by Joesph W. Jewel et al.

Title:	Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98
Author:	Jewel, Joesph W.
Author:	Langley Research Center
Note:	National Aeronautics and Space Administration, 1960

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Subject:	Aerodynamic drag
Subject:	Aerodynamic noise
Subject:	Compressibility effects
Subject:	Helicopter performance
Subject:	Helicopter wakes
Subject:	Hovering
Subject:	Lift
Subject:	Mach number
Subject:	Pressure
Subject:	Rotary wings
Subject:	Rotor speed
Subject:	Sound
Subject:	Subsonic speed
Subject:	Thrust
Subject:	Tip speed
Subject:	Wind tunnel tests
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