<--- Back to Details
First PageDocument Content
Oswald efficiency number / Wing configuration / Drag / Lift-to-drag ratio / Lift / Closed wing / Lifting-line theory / Washout / Aerospace engineering / Aerodynamics / Lift-induced drag
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

Task_h_b_variations_2012-04-24

Add to Reading List

Source URL: www.fzt.haw-hamburg.de

Download Document from Source Website

File Size: 63,31 KB

Share Document on Facebook

Similar Documents

Aerodynamics / Wingtip device / Airfoil / Lift-induced drag / Camber / Lift / Foil / Angle of attack / Swept wing / Chord / Propeller / Stall

Microsoft Word - EXHIBIT A.doc

DocID: 1pI3W - View Document

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

DocID: 195q0 - View Document

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

DocID: 18Acm - View Document

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

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

DocID: 18r7b - View Document

Oswald efficiency number / Wing configuration / Drag / Lift-to-drag ratio / Lift / Closed wing / Lifting-line theory / Washout / Aerospace engineering / Aerodynamics / Lift-induced drag

Task_h_b_variations_2012-04-24

DocID: 17Kv2 - View Document