Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA 64(1)-212
Filename
n64212.dat
t/c
12.0%
Max Camber
1.1%
Download Selig Coordinates
Run in Airfoil Model
Quick Analysis
Reynolds Number
i
Include Mach Number
i
Yes
No
Website (leave this field empty)
Run
Errors & Warnings
Similar Airfoils
MH 108 11.98%
t/c 12.0% · Max Camber 1.1%
NACA 63-212
t/c 12.0% · Max Camber 1.1%
NACA 65(1)-212
t/c 12.0% · Max Camber 1.1%
NACA 66(1)-212
t/c 12.0% · Max Camber 1.1%
NASA SC(2)-0612
t/c 12.0% · Max Camber 1.1%
GOE 780
t/c 12.0% · Max Camber 1.0%