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Serrated-Planform Lifting-SurfacesA novel set of serrated-planform lifting surfaces produce unexpectedly high lift coefficients at moderate to high angles-of-attack. Each serration, or tooth, is designed to shed a vortex. The interaction of the vortices greatly enhances the lifting capability over an extremely large operating range. Variations of the invention use serrated-planform lifting surfaces in planes different than that of a primary lifting surface. In an alternate embodiment, the individual teeth are controllably retractable and deployable to provide for active control of the vortex system and hence lift coefficient. Differential lift on multiple serrated-planform lifting surfaces provides a means for vehicle control. The important aerodynamic advantages of the serrated-planform lifting surfaces are not limited to aircraft applications but can be used to establish desirable performance characteristics for missiles, land vehicles, and/or watercraft.
Document ID
20000025500
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
McGrath, Brian E.
(NASA Langley Research Center Hampton, VA United States)
Wood, Richard M.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
May 11, 1999
Subject Category
Aerodynamics
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-734820
Patent Number: US-Patent-5,901,925
Patent Number: NASA-Case-LAR-15295-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-5,901,925|NASA-Case-LAR-15295-1
Patent Application
US-Patent-Appl-SN-734820
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