Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
DAE-11
Filename
dae11.dat
t/c
12.8%
Max Camber
6.6%
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 114 13.02%
t/c 13.1% · Max Camber 6.6%
GOE 501
t/c 12.8% · Max Camber 6.3%
GOE 446
t/c 12.9% · Max Camber 6.3%
Fage & Collins 4
t/c 12.7% · Max Camber 6.3%
GOE 528
t/c 12.5% · Max Camber 6.2%
N-22
t/c 12.4% · Max Camber 6.2%