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.
Airfoils for Light Transport Aircraft
Sae Technical Papers
Business Aircraft Meeting and Exposition ; 1981
1981-02-01
Conference paper
English
Laminar-Airfoils for Transport Aircraft
NTIS | 1980
|Laminar Airfoils for Transport Aircraft
NTIS | 1981
|Aircraft with Single Surface Membranous Airfoils
NTIS | 1985
|Choice of airfoils for rotating-wing aircraft
Engineering Index Backfile | 1934
|