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Date: 2014-06-09 16:38:04Aerodynamics 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 EfficiencyAdd to Reading ListSource URL: rotorcraft.arc.nasa.govDownload Document from Source WebsiteFile Size: 2,13 MBShare Document on Facebook |