NM Spatz tip for 50% ailerons DB Name: NM Spatz tip for 50% ailerons Family: Mathis Max thickness: 12.2% at x = 21.48% chord Max camber: 2.5% at x = 28.25% 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. http://kipecoul.e-monsite.com/pages/profil-vieille-plume/profil-avec-extrados-et-intrados-plat.html