Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Reexamination Certificate
2011-08-09
2011-08-09
Michener, Joshua J (Department: 3644)
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
C244S03500A, C244S217000
Reexamination Certificate
active
07992827
ABSTRACT:
A wing for an aircraft is provided, including at least a first wing portion configured for providing high-lift mild stall characteristics at least at Reynolds numbers in the range between about 0.3*106and about 2.0*106, and at least a second wing portion comprising a substantially permanently slotted aerofoil arrangement. Also provided are an air vehicle including such wings, a method for operating an aircraft, and a method for designing an aircraft wing.
REFERENCES:
patent: 4072282 (1978-02-01), Fulker et al.
patent: 6382921 (2002-05-01), Selig et al.
patent: 6607164 (2003-08-01), Somers
patent: 7048228 (2006-05-01), Vassberg et al.
patent: 605765 (1948-07-01), None
Nagel et al., The Concept of High-Lift, Mild Stall Wing, 2004, ICAS.
Nagel Alex
Shepshelovich Michael
Hopkins Susanne M.
Israel Aerospace Industries Ltd.
Klima William L.
Michener Joshua J
The Nath Law Group
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