An S1210 profile aerofoil of 60mm chord for use with the AF1300 Subsonic Wind Tunnel.
An unsymmetrical aerofoil that spans the full width of the working section of the Subsonic Wind Tunnel (AF1300), for two-dimensional experiments. This aerofoil has an S1210 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.
AF1300S - Package
A starter set consisting of the Subsonic Wind Tunnel 305 mm (AF1300), Basic Lift and Drag Balance (AF1300z) and a set of Three-Dimensional Drag Models (AF1300j).
Digital differential pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnel (AF1300).
A traversing Pitot static tube with electronic position measurement for use with TecQuipment’s Subsonic Wind Tunnels (AF1300, AF1300s, AF1600s).
A two-component balance that measures lift and drag forces on models mounted in the AF1300 Subsonic Wind Tunnel.
Supports wind tunnel models in the AF1300 Subsonic Tunnel and measures their lift, drag and pitching moment.
Allows students to investigate the direct and indirect measurement of drag on various shapes and to calculate and analyse the drag coefficient by different methods.
AF1300R - Experiment
An aerofoil suspended on springs within a frame, used to demonstrate wing flutter. The suspension positions of the wing can be altered, as can the angle of attack.