Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA 64-210
Filename
naca64210.dat
t/c
10.0%
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 110 10.01%
t/c 10.0% · Max Camber 1.1%
NACA 63-210
t/c 10.0% · Max Camber 1.1%
NACA 65-210
t/c 10.0% · Max Camber 1.1%
NACA 66-210
t/c 10.0% · Max Camber 1.1%
NASA/AMES A-03
t/c 10.0% · Max Camber 1.2%
NASA SC(2)-0410
t/c 10.0% · Max Camber 1.2%