Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
RAE(NPL) 5212
Filename
rae5212.dat
t/c
11.9%
Max Camber
1.8%
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 23012 12%
t/c 12.0% · Max Camber 1.8%
GOE 676 (= M 12)
t/c 11.9% · Max Camber 2.0%
NACA M12
t/c 11.9% · Max Camber 2.0%
NACA M12
t/c 11.9% · Max Camber 2.0%
S8052
t/c 11.9% · Max Camber 1.6%
TsAGI 12%
t/c 11.9% · Max Camber 2.0%