MID 101 Family: Midic Max thickness: 7.7% at x = 19.90% chord Max camber: 4.5% at x = 51.95% chord Available data sources: JavaFoil+Calcfoil stall+Eppler ext transition
Notes:
Coordinates from TraCFoil. Commercial use of the airfoil may be restricted by the designer's copyright. For F1A as low drag airfoils.