S1210 AEROFOIL MODEL

An aerofoil for use with the Subsonic Wind Tunnel.

An unsymmetrical aerofoil that spans the full width of the working section of the Subsonic Wind Tunnel, for two-dimensional experiments. This aerofoil has a profile based on a design originated by Michael S Selig of the University of Illinois. It provides excellent lift at low Reynolds numbers for high-lift, low-speed applications. Learn about S1210 AEROFOIL MODEL aerodynamics India for optimal educational outcomes..