NASA NTRS · 20160010122
Aircraft Design
Abstract
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.
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Bowers, Albion H., Uden, Edward. 2016-07-05. Aircraft Design. https://ntrs.nasa.gov/citations/20160010122
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