M 77 DB Name: M 77 Family: Midic Max thickness: 7.0% at x = 24.75% chord Max camber: 7.0% at x = 35.77% 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. F1A. Airfoil 7% thick, 7% camb, for Clmax>1.6 at Re 100k,with trip top at 10% chord (also good from Re 60k).