Five drag investigation models for use with the TecQuipment AF1300 wind tunnel - a streamlined shape, a sphere, hemisphere, "dimpled" sphere, and a flat plate. All the models have a 50mm frontal area for easy comparison
A set of different shape models with identical frontal area to allow students to compare the different coefficient of drag for each shape. Includes a dummy stem for tests to cancel out the drag due to each model’s support arm.
Note: You also need the optional two or three component balance (AF1300z or AF1300t) for direct readings of drag.
Supports wind tunnel models in the AF1300 Subsonic Tunnel and measures their lift, drag and pitching moment.
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.
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.