Oswald efficiency number

#	Item
1	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 Distribution Add to Reading List Source URL: www.fzt.haw-hamburg.de Language: English - Date: 2012-07-08 06:04:33 Oswald efficiency number Drag Aspect ratio Lift-to-drag ratio Wingtip device Wing configuration Closed wing Wing loading Chord Aerospace engineering Aerodynamics Lift-induced drag
2	Task_h_b_variations_2012-04-24 Add to Reading List Source URL: www.fzt.haw-hamburg.de Language: English - Date: 2012-04-24 05:00:39 Oswald efficiency number Wing configuration Drag Lift-to-drag ratio Lift Closed wing Lifting-line theory Washout Aerospace engineering Aerodynamics Lift-induced drag
3	PDF Document Add to Reading List Source URL: pdf.aiaa.org Language: English - Date: 2009-11-12 17:12:50 Space technology Dimensionless numbers Force Propulsive Wing Lift coefficient Airfoil Pressure coefficient Oswald efficiency number Lift Aerodynamics Aerospace engineering Fluid dynamics