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Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98

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:
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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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