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Slotted Aircraft WingAn aircraft wing includes a leading airfoil element and a trailing airfoil element. At least one slot is defined by the wing during at least one transonic condition of the wing. The slot may either extend spanwise along only a portion of the wingspan, or it may extend spanwise along the entire wingspan. In either case, the slot allows a portion of the air flowing along the lower surface of the leading airfoil element to split and flow over the upper surface of the trailing airfoil element so as to achieve a performance improvement in the transonic condition.
Document ID
20060049149
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Vassberg, John C.
Gea, Lie-Mine
McLean, James D.
Witowski, David P.
Krist, Steven E.
Campbell, Richard L.
Date Acquired
August 23, 2013
Publication Date
May 23, 2006
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-678474
Patent Number: NASA-Case-LAR-16517-1
Patent Number: US-Patent-7,048,228
Patent Application Number: US-Patent-Appl-SN-417355
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-LAR-16517-1|US-Patent-7,048,228
Patent Application
US-Patent-Appl-SN-678474|US-Patent-Appl-SN-417355
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