Max thickness: 9.6% at x = 26.46% chord
Max camber: 2.0% at x = 24.73% 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.
Airfoils for Blended body configuration - MID 371 AW at root, MID 371 at tip, and interpolates airfoils between.