Back to Results
First PageMeta Content
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

Document Date: 2012-04-24 05:00:39

Open Document

File Size: 63,31 KB

Share Result on Facebook

Company

Airbus / /

IndustryTerm

aerodynamics software / /

Product

Airbus A320 / /

SocialTag