Max thickness: 7.7% at x = 21.46% chord
Max camber: 4.5% at x = 51.95% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
Coordinates from TraCFoil.
Commercial use of the airfoil may be restricted by the designer's copyright.
This airfoil was develope from two my diffrente airfoils:
bottom side is from airfoil MID 103 and upper side is
from MID 106, both developed separately earlier. New
hybrid airfoil MID 104 has thickness of 7.74%, and camber
of 4.5%. It is intended for all free flite (FF) airplane models
for low speed with Re numbers from 40,000 and more.