Subsonic Wind Tunnels
BALANCE ANGLE FEEDBACK
Measures angular positions of models mounted on TecQuipment’s Three- Component Balance (AF1300T, AF1450T or AF1600T) with the Versatile Data Acquisition System (VDAS®).
THREE COMPONENT BALANCE
A three-component balance designed for use with the AF1300 Subsonic Wind Tunnel.
MULTI-TUBE MANOMETER
A tilting 36-tube manometer for use with the AF1300, AF1450 and AF1600 Subsonic Wind Tunnels, other TecQuipment products, or as a general purpose instrument.
S1210 AEROFOIL MODEL
An S1210 profile aerofoil of 150 mm chord for use with the AF1300 Subsonic Wind Tunnel.
THREE DIMENSIONAL DRAG MODELS
Five drag investigation models for use with the TecQuipment AF1300 wind tunnel - a streamlined shape, a sphere, hemisphere, "dimpled" sphere, and a flat plate. All the models have a 50mm frontal area for easy comparison
AIRCRAFT MODEL HIGH WING
A model aircraft with high wing configuration for use in TecQuipment's AF1300 Wind Tunnel.
AIRCRAFT MODEL LOW WING
A model aircraft with low wing configuration for use in TecQuipment's AF1300 Wind Tunnel.
BOUNDARY LAYER MODEL
A flat boundary layer model to illustrate the phenomena of boundary layer development and separation. For use with the AF1300 Subsonic Wind Tunnel.
FLAT PLATE DRAG MODEL
A 100 mm diameter flat plate for use with the AF1300 Subsonic Wind Tunnel.
SET OF 2 NACA 0012 AEROFOIL MODELS
A set of two aerofoils both of NACA0012 profile and 150 mm chord for use with the AF1300 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 AF1300 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 AF1300 Subsonic Wind Tunnel.