DB Name: MID 027
Max thickness: 5.1% at x = 21.45% chord
Max camber: 2.5% at x = 56.00% 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.
Re ~10k-40k HL Glider