Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1982-03-09
1985-02-12
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244216, 416223R, B64C 326
Patent
active
044986467
ABSTRACT:
Profile design for aircraft lift-wings in general aviation up to flight speeds of about 700 km/h, the profile design being determined by the path of the center line with a forward (first) and rear (second) camber maximum and with a profile droplet superposed on the center line and of a specific thickness distribution, and by the design of the profile nose to have a relatively small nose radius and relatively strong camber.
REFERENCES:
patent: 3576301 (1971-04-01), Stickle
patent: 4121787 (1978-10-01), Wilby
patent: 4413796 (1983-11-01), Bousquet
Lotz, deceased Michael
Proksch Hans-Jorg
Welte Dieter
Zimmer Herbert
Barefoot Galen L.
Dornier GmbH
Siegemund Ralf H.
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