AF1600S
AF1450S
AF1300
AF1125
Size comparison of the subsonic wind tunnels range
Subsonic Wind Tunnel 305 mm AF1300 A compact, free-standing, open-circuit suction subsonic wind tunnel with a working section of 305 mm by 305 mm and 600 mm long, allowing
students to perform advanced study such as analysing boundary layers, performing flow visualisation and observing velocity in the wake, offering
extensive teaching
and research functionality.
DATASHEET
Base Unit (af1300)
Instrumentation
available Experiments
available experiments: • Cylinder Model with Tapping (AF1300a) • NACA 0012 Aerofoil with Tappings (AF1300b) • NACA 2412 Aerofoil with Flap (AF1300c) • Set of Two NACA 0012 Aerofoils (AF1300d) • Set of Four NADA Aerofoils (AF1300d2)
• Aircraft Model (Low Wing) (AF1300g) • Aircraft Model (High Wing) (AF1300h) • Three-Dimensional Drag Models (AF1300j)
Winglets and end plates
• S1210 Aerofoil (AF1300l) • Swept Wing (AF1300l2*) • Winglets and End Plates (AF1300q)
• Set of Two Blades (AF1300d3*) • Flat Plate Drag Model (AF1300e) • Boundary Layer Model (AF1300f)
• Flutter Wing (AF1300r) *Compatible with DefleX ®
Flutter wing
A starter set is available consisting of the Subsonic Wind Tunnel 305 mm (AF1300), Basic Lift and Drag Balance (AF1300z) and a set of Three-Dimensional Drag Models (AF1300j).
DATASHEET
DefleX® Camera Mount AF1300DCS A simple mount that allows the DefleX ® camera unit to be used with the AF1300 Subsonic Wind Tunnel.
experiments and instrumentation poster
Instrumentation requirement chart
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+44 115 972 2611
Info@tecquipment.com
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