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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
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Document Date: 2014-06-09 16:38:04

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File Size: 2,13 MB

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