Task_h_b_variations_2012-04-24

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Date: 2012-04-24 05:00:39 Oswald efficiency number Wing configuration Drag Lift-to-drag ratio Lift Closed wing Lifting-line theory Washout Aerospace engineering Aerodynamics Lift-induced drag		Task_h_b_variations_2012-04-24 Add to Reading List Source URL: www.fzt.haw-hamburg.de Download Document from Source Website File Size: 63,31 KB Share Document on Facebook

	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 DocID: 18r7b - View Document
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