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Aircraft DesignThe 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.
Document ID
20160010122
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Bowers, Albion H.
Uden, Edward
Date Acquired
August 8, 2016
Publication Date
July 5, 2016
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-14/297,186
Patent Number: US-Patent-9,382,000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,382,000
Patent Application
US-Patent-Appl-SN-14/297,186

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