VANE 15% gap 1% Family: Midic Max thickness: 15.0% at x = 26.50% chord Max camber: 0.0% at x = 0.00% 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. For low Re, trip top & bottom @ 30% chord.