MID 104 DB Name: MID 104 Family: Midic 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 XFOIL ncrit=9
Notes:
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.