Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA M16
Filename
m16.dat
t/c
6.2%
Max Camber
4.1%
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
GOE 393
t/c 6.1% · Max Camber 4.2%
NACA M13
t/c 6.2% · Max Camber 3.9%
GOE 372
t/c 6.2% · Max Camber 4.3%
HAM-STD HS1-606
t/c 6.0% · Max Camber 4.2%
Coanda 2
t/c 6.0% · Max Camber 4.3%
GOE 142 (MVA H.19)
t/c 6.2% · Max Camber 3.8%