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
An optional experiment module for use with the AF10 Air Flow Bench. For students to study boundary layers on rough and smooth flat plates. Includes a pitot to measure velocity profiles. Also allows experiments with pressure gradients.
BASIC LIFT AND DRAG BALANCE
A two-component balance to measure the lift and drag forces on models mounted in an 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, AF1450, AF1600).
32 WAY PRESSURE DISPLAY UNIT
The 32-Way Pressure Display Unit displays up to 32 different pressures from models Pitot-static tubes and other measuring instruments fitted to a wind tunnel.
DIFFERENTIAL PRESSURE UNIT
Digital differential pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnel (AF1300).