Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
GOE 411
Filename
goe411.dat
t/c
13.2%
Max Camber
0.0%
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
NASA/LANGLEY LS(1)-0013
t/c 12.9% · Max Camber 0.0%
St. CYR 172 (Royer)
t/c 13.6% · Max Camber 0.0%
ULTIMATE
t/c 12.8% · Max Camber -0.3%
GOE 409
t/c 12.7% · Max Camber 0.0%
GOE 459
t/c 12.7% · Max Camber 0.0%
DU 86-137/25
t/c 13.6% · Max Camber 0.3%
