Aerodule
Hardware
Engineering Models
Documentation
Pricing
Contact
Sign In
← Airfoil Catalog
MH 114 13.02%
Filename
mh114.dat
t/c
13.1%
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
DAE-11
t/c 12.8% · Max Camber 6.6%
GOE 446
t/c 12.9% · Max Camber 6.3%
GOE 501
t/c 12.8% · Max Camber 6.3%
Fage & Collins 4
t/c 12.7% · Max Camber 6.3%
Dayton-Wright T-1
t/c 13.4% · Max Camber 7.1%
GOE 322 (HANSA-BRANDENBURG IV.1)
t/c 13.1% · Max Camber 6.0%
