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)
• Flat Plate Drag Model (AF1300e) • Boundary Layer Model (AF1300f)
Winglets and end plates
Instrumentation requirement chart
• Aircraft Model (Low Wing) (AF1300g) • Aircraft Model (High Wing) (AF1300h) • Three-Dimensional Drag Models (AF1300j) • S1210 Aerofoil (AF1300l) • Winglets and End Plates (AF1300q) • Flutter Wing (AF1300r)
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
experiments and instrumentation poster
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