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Airfoils for Light Transport Aircraft

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Poole, R.J.D., author.
Conference Name:
Business Aircraft Meeting and Exposition (1981-04-07 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1981
Summary:
This paper presents data from tests in a two-dimensional pressurized wind tunnel of two new wing sections suitable for light transport aircraft, and a NACA 633-418 airfoil. The two new airfoils had maximum thickness/chord ratios of 18% and 21% and they were designed to achieve improved high lift and low drag by exploiting considerable aft loading and blunt trailing edges
Notes:
Vendor supplied data
Publisher Number:
810576
Access Restriction:
Restricted for use by site license

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