The present invention is an aircraft wing design that creates a bell shaped span load, which results in a negative induced drag (induced thrust) on the outer portion of the wing; such a design obviates the need for rudder control of an aircraft.
Aircraft Design
2016-07-05
Miscellaneous
No indication
English
AIRCRAFT DESIGN METHOD, AIRCRAFT DESIGN PROGRAM AND AIRCRAFT DESIGN DEVICE
European Patent Office | 2016
|TIBKAT | 2010
|Online Contents | 2009
Online Contents | 1996
TIBKAT | 2010
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