An S1210 profile aerofoil of 150 mm 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 (AF100), 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
An open circuit suction subsonic wind tunnel with a working section of 300 mm by 300 mm and 600 mm long.
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, AF1450, AF1600).
A two-component balance to measure the lift and drag forces on models mounted in an AF1300 Subsonic Wind Tunnel.
A three-component balance designed for use with the AF1300 Subsonic Wind Tunnel.
An experimental module for use with the AF10 Air Flow Bench to provide experiments that measure and compare the effects of drag force on objects mounted in an airstream that have the same projected frontal area but different shape. Facilities to compare drag force measurement methods are included.
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.