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Date: 2012-06-24 14:53:00Aircraft Wing configuration Swept wing Aspect ratio Lift-induced drag Fixed-wing aircraft Lift-to-drag ratio Biplane Chord Aerospace engineering Aerodynamics Aviation | Deutscher Luft- und Raumfahrtkongress 2011 DocumentID: BOX WING FUNDAMENTALS – AN AIRCRAFT DESIGN PERSPECTIVE D. Schiktanz, D. Scholz Hamburg University of Applied SciencesAdd to Reading ListSource URL: www.fzt.haw-hamburg.deDownload Document from Source WebsiteFile Size: 603,83 KBShare Document on Facebook |
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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 | |
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