Max thickness: 8.5% at x = 31.92% chord
Max camber: 1.1% at x = 39.72% 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.
Well suited for 20% chord flaps.
Can be used at Re of 150k and above.
At Re below 150k, a turbulator should be placed at 75% chord.