Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
E209
Filename
e209.dat
t/c
13.7%
Max Camber
2.0%
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
GOE 617
t/c 13.9% · Max Camber 2.2%
LOCKHEED L-188 ROOT
t/c 14.0% · Max Camber 2.0%
NACA 2414
t/c 14.0% · Max Camber 2.0%
DFVLR R-4
t/c 13.4% · Max Camber 2.1%
Falcon
t/c 13.7% · Max Camber 1.6%
SC(2)-0714
t/c 13.9% · Max Camber 1.5%