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Date: 2012-04-24 05:00:39Oswald 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_2012-04-24Add to Reading ListSource URL: www.fzt.haw-hamburg.deDownload Document from Source WebsiteFile Size: 63,31 KBShare Document on Facebook |