Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
MI-VAWT1
Filename
mi-vawt1.dat
t/c
21.0%
Max Camber
0.4%
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 775
t/c 21.0% · Max Camber 0.2%
NACA 66-021
t/c 21.0% · Max Camber 0.0%
NACA 0021
t/c 21.0% · Max Camber 0.0%
NACA 16-021
t/c 21.0% · Max Camber 0.0%
GOE 460
t/c 20.5% · Max Camber 0.0%
NACA 63(4)-221
t/c 21.0% · Max Camber 1.1%
