Flutter Wing Experiment
Product Overview - Flutter Wing
Experiment Overview - Flutter Wing
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.
An open circuit suction subsonic wind tunnel with a working section of 300 mm by 300 mm and 600 mm long.
Measures angular positions of models mounted on TecQuipment’s Three- Component Balance (AF1300T, AF1450T or AF1600T) with the Versatile Data Acquisition System (VDAS®).
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 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.
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