Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
HQ 2.5/11
Filename
hq2511.dat
t/c
11.0%
Max Camber
2.5%
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 2.5411
t/c 11.0% · Max Camber 2.5%
BOEING-VERTOL VR-11X
t/c 11.0% · Max Camber 2.4%
E211
t/c 10.9% · Max Camber 2.6%
DF 101
t/c 11.0% · Max Camber 2.3%
DF102
t/c 11.0% · Max Camber 2.3%
DSMA-523A
t/c 11.0% · Max Camber 2.3%