Results of flight tests indicate that profile-drag coefficients which were obtained with the low-drag airfoils were lower than with the conventional types over the range of light coefficients tested. For comparable conditions of the lift coefficient and Reynolds Number, the low-drag airfoils have profile-drag coefficients which may be 27 percent lower than the profile drag of the conventional airfoils tested. Detailed results are presented graphically.
Profile-Drag Coefficients of Conventional and Low-Drag Airfoils as Obtained in Flight
1944-05-01
Sonstige
Keine Angabe
Englisch
AIRFOILS - NACA - CHARACTERISTICS LOW-DRAG , Aerodynamics , AIRFOILS - NACA 64,2-(1 4) (13 5) LOW-DRAG CHARACTERISTICS , AIRFOILS - REPUBLIC S-3,13 - CHARACTERISTICS , AIRFOILS - NACA 27-212 - CHARACTERISTICS LOW-DRAG , AIRFOILS - NACA 35-215 - CHARACTERISTICS LOW-DRAG , AIRFOILS - NACA 2414 5 - CHARACTERISTICS , DRAG, PROFILE - MEASUREMENT , AIRFOILS - REPUBLIC S-3,11 - CHARACTERISTICS , AIRFOILS - NAVY N-22 - CHARACTERISTICS , AIRFOILS - NACA 66, 2-2(14 7) - CHARACTERISTICS LOW-DRAG
Profile-drag coefficients of conventional and low-drag airfoils as obtained in flight
Engineering Index Backfile | 1944
|Engineering Index Backfile | 1948
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