Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA 66-206
Filename
naca66206.dat
t/c
6.0%
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
NACA 63-206
t/c 6.0% · Max Camber 1.1%
NACA 64-206
t/c 6.0% · Max Camber 1.1%
NACA 65-206
t/c 6.0% · Max Camber 1.1%
BOEING VERTOL V13006-.7
t/c 6.0% · Max Camber 0.9%
ONERA OA206
t/c 6.0% · Max Camber 0.8%
HT23
t/c 6.5% · Max Camber 1.1%