Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA 65(3)-218
Filename
naca653218.dat
t/c
18.0%
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(3)-218
t/c 18.0% · Max Camber 1.1%
NACA 64(3)-218
t/c 18.0% · Max Camber 1.1%
NACA 66(3)-218
t/c 18.0% · Max Camber 1.1%
AS5048
t/c 18.0% · Max Camber 1.2%
NASA SC(2)-0518
t/c 18.0% · Max Camber 1.5%
NACA 23018
t/c 18.0% · Max Camber 1.8%
