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Longitudinal static stability / Pitching moment / Fixed-wing aircraft / Lift-induced drag / Biplane / Wing loading / Aircraft / Aspect ratio / Gliding flight / Aerospace engineering / Aerodynamics / Aviation


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
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Document Date: 2012-06-24 15:02:14


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File Size: 1,96 MB

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