Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency

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Date: 2014-06-09 16:38:04 Aerodynamics Disk loading Rotorcraft Tiltrotor Helicopter Wingtip device Wing loading Lift-to-drag ratio Lift-induced drag Aerospace engineering Aircraft Aviation		Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency Add to Reading List Source URL: rotorcraft.arc.nasa.gov Download Document from Source Website File Size: 2,13 MB Share Document on Facebook

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