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 K - Lift-induced drag - Document - PDFSEARCH.IO

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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 K Add to Reading List Document Date: 2012-06-24 15:02:14 Open Document File Size: 1,96 MB Share Result on Facebook Company D. Scholz Aero / Airbus / / Facility Hamburg University of Applied Sciences / / IndustryTerm closed wing systems / energy / / Organization Lift Division / Hamburg University of Applied Sciences / Hamburg / / Person Flightpath / / Position far forward / region forward / / Product Airbus A320 / winglet / biplane / / Technology 2050 technologies / / SocialTag Longitudinal static stability Pitching moment Fixed-wing aircraft Lift-induced drag Biplane Wing loading Aircraft Aspect ratio Gliding flight Aerospace engineering

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 KAdd to Reading List