Deutscher Luft- und Raumfahrtkongress 2011 DocumentID: BOX WING FUNDAMENTALS – AN AIRCRAFT DESIGN PERSPECTIVE D. Schiktanz, D. Scholz Hamburg University of Applied Sciences - Lift-to-drag ratio - Document - PDFSEARCH.IO

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Date: 2012-06-24 14:53:00 Aircraft 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 Sciences Add to Reading List Source URL: www.fzt.haw-hamburg.de Download Document from Source Website File Size: 603,83 KB Share Document on Facebook

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