Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
NACA M4
Filename
m4.dat
t/c
6.3%
Max Camber
2.2%
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
USA 46
t/c 6.5% · Max Camber 2.2%
AG03 (flat aft bottom)
t/c 6.2% · Max Camber 2.0%
GOE 55
t/c 6.2% · Max Camber 2.0%
AG17
t/c 6.5% · Max Camber 2.0%
AG46c -03f
t/c 6.0% · Max Camber 2.3%
RAF 26
t/c 6.6% · Max Camber 2.1%