Flight Demonstration Wind Tunnel AF41V
DATASHEET
A model aircraft suspended in an open circuit wind tunnel. Includes realistic fly-by-wire flight controls to simulate a variety of principles of aircraft flight.
Intermittent Supersonic Wind Tunnel AF300 An intermittent supersonic (up to Mach 1.8) wind tunnel for investigations into subsonic and supersonic air flow around two-dimensional models. Also for analysis of the profile of the tunnel working section.
DATASHEET
Continuous Supersonic WIND TUNNEL AF302 A suction-type, continuous-operation supersonic (up to Mach 1.8) wind tunnel for investigations into subsonic and supersonic air flow around
two-dimensional models. Also for analysis of the profile of the tunnel working section.
DATASHEET
Schlieren Apparatus AF300a / AF302a The Schlieren apparatus enables students to see air flow (including supersonic shock waves) around two-dimensional models as variations in the intensity of illumination. For use with the Intermittent (AF300) and Continuous (AF302) Supersonic Wind Tunnels.
5 degrees mach 1-8 and 5 degree wedge
DATASHEET
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+44 115 972 2611
Info@tecquipment.com
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