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Laminar-flow airfoilAn airfoil having a fore airfoil element, an aft airfoil element, and a slot region in between them. These elements induce laminar flow over substantially all of the fore airfoil element and also provide for laminar flow in at least a portion of the slot region. The method of the invention is one for inducing natural laminar flow over an airfoil. In the method, a fore airfoil element, having a leading and trailing edge, and an aft airfoil element define a slot region. Natural laminar flow is induced over substantially all of the fore airfoil element, by inducing the pressures on both surfaces of the fore airfoil element to decrease to a location proximate the trailing edge of the fore airfoil element using pressures created by the aft airfoil element.
Document ID
20080005076
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Somers, Dan M.
Date Acquired
August 24, 2013
Publication Date
June 14, 2005
Subject Category
Aerodynamics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-299660
Patent Number: US-PATENT-6,905,092
Funding Number(s)
CONTRACT_GRANT: NAS1-01076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,905,092
Patent Application
US-PATENT-APPL-SN-299660
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