Family: NACA 4-digit
Max thickness: 11.0% at x = 30.06% chord
Max camber: 2.5% at x = 39.72% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
Wind Tunnel (SoarTech 8)
The NACA2.4511 is a NACA four-digit section with 2.5% maximum camber at 40% chord, and 11% thickness.
Coordinates from SoarTech 8.
Wind tunnel data from the UIUC Low-Speed Airfoil Test Program.
The UIUC wind tunnel data is covered by the GNU GPL and the airfoil performance data is copyrighted, and restrictions are placed on its use.
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