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Oswald efficiency number / Drag / Aspect ratio / Lift-to-drag ratio / Wingtip device / Wing configuration / Closed wing / Wing loading / Chord / Aerospace engineering / Aerodynamics / Lift-induced drag


Project Department of Automotive and Aeronautical Engineering The Effect of Variations of the Height to Span Ratio of Box Wing Aircraft on Induced Drag and the Spanwise Lift Distribution
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Document Date: 2012-07-08 06:04:33


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