Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA 63(3)-618
Filename
naca633618.dat
t/c
18.0%
Max Camber
3.3%
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 65(3)-618
t/c 18.0% · Max Camber 3.3%
RONCZ 1080 VOYAGER INNER AFT WING
t/c 18.0% · Max Camber 3.3%
RONCZ 1082 VOYAGER ROOT OUTER AFT WING
t/c 18.0% · Max Camber 3.4%
NACA 64(3)-618
t/c 17.9% · Max Camber 3.3%
HQ 3.5/18
t/c 18.0% · Max Camber 3.5%
CLARK YM-18
t/c 18.0% · Max Camber 3.6%
