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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 | Add to Reading List |
![]() | Microsoft Word - EXHIBIT A.docDocID: 1pI3W - View Document |
![]() | The Conflict of Aerodynamic Efficiency and Static Longitudinal Stability of Box Wing Aircraft D. Schiktanz, D. Scholz Aero – Aircraft Design and Systems Group, Hamburg University of Applied Sciences, Hamburg, Germany KDocID: 195q0 - View Document |
![]() | Deutscher Luft- und Raumfahrtkongress 2011 DocumentID: BOX WING FUNDAMENTALS – AN AIRCRAFT DESIGN PERSPECTIVE D. Schiktanz, D. Scholz Hamburg University of Applied SciencesDocID: 18Acm - View Document |
![]() | 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 DistributionDocID: 18r7b - View Document |
![]() | Task_h_b_variations_2012-04-24DocID: 17Kv2 - View Document |