Subsonic Wind Tunnels
AIRCRAFT MODEL LOW WING
A model aircraft with low wing configuration for use in TecQuipment's AF1450 Wind Tunnel.
FLAT PLATE BOUNDARY LAYER MODEL
A flat boundary layer model to illustrate the phenomena of boundary layer development and separation. For use with the AF1450 Subsonic Wind Tunnel.
FLAT PLATE DRAG MODEL
A 100 mm diameter flat plate for use with the AF1450 Subsonic Wind Tunnel.
SET OF 2 NACA 0012 AEROFOILS
A set of two aerofoils both of NACA0012 profile and 150 mm chord for use with the AF1450 Subsonic Wind Tunnel.
NACA 2412 AEROFOIL MODEL WITH FLAP
A 150 mm chord NACA2412 unsymmetrical section aerofoil with 300 mm span and adjustable flap for use with the AF1450 Subsonic Wind Tunnel.
NACA 0012 AEROFOIL MODEL WITH TAPPINGS
A 150 mm chord 300 mm span NACA0012 aerofoil with pressure tappings for use with the AF1450 Subsonic Wind Tunnel.
CYLINDER MODEL
A cylinder model with a single pressure tapping point for use with the AF1450 Subsonic Wind Tunnel.
BOUNDARY LAYER
Allows students to investigate both the laminar and turbulent boundary layers on flat plates with rough and smooth surfaces.
BASIC LIFT AND DRAG BALANCE
A two-component balance that measures lift and drag forces on models mounted in the AF1300 Subsonic Wind Tunnel.
PITOT STATIC TRAVERSE (DIGITAL)
A traversing Pitot static tube with electronic position measurement for use with TecQuipment’s Subsonic Wind Tunnels (AF1300, AF1300s, AF1600s).
32 WAY PRESSURE DISPLAY UNIT
A 32-way pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnels (AF1300, AF1300s, AF1450s, AF1600s).
DIFFERENTIAL PRESSURE TRANSDUCER
Digital differential pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnel (AF1300).