Airfoil:

mm

Job Status

Please wait while the PDF is generated...

Plot Number:

File:

Search for Airfoil
Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
NACA 4403 3.03 34.5328 3.971 42.2134 0.896 0.0051
View
NACA 4412 12.02 30 3.943 40 1.649 0.0029
View
NACA 4415 14.99 30 3.939 40 1.588 0.0058
View
NACA 4418 18 30 3.934 40 1.551 0.0104
View
NACA 4508 8.11 27.03 3.925 48.44 0.94 0.0053
View
V 1.0