AF1300H - Experiment

AIRCRAFT MODEL HIGH WING

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A model aircraft with high wing configuration for use in TecQuipment's AF1300 Wind Tunnel.

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AIRCRAFT MODEL HIGH WING

Model aircraft with NACA profile wings. One has a low wing position (bottom of the fuselage), the other has a high wing position (above the fuselage). These models are good for experiments with lift, drag and pitching moment of fixed wing aircraft.

AIRCRAFT MODEL HIGH WING
SUPPORTING PRODUCTS
VDAS AF1300S - Package

An open circuit suction subsonic wind tunnel with a working section of 300 mm by 300 mm and 600 mm long.

AF1300T - Ancillary

A three-component balance designed for use with the AF1300 Subsonic Wind Tunnel.

VDAS AF1300R - Experiment

An aerofoil suspended on springs within a frame, used to demonstrate wing flutter. The suspension positions of the wing can be altered, as can the angle of attack.

AF1300G - Experiment

A model aircraft with low wing configuration for use in TecQuipment's AF1300 Wind Tunnel.

AFA4 - Ancillary

Measures angular positions of models mounted on TecQuipment’s Three- Component Balance (AF1300T, AF1450T or AF1600T) with the Versatile Data Acquisition System (VDAS®).

AFA5 - Ancillary

Digital differential pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnel (AF1300).

AFA7 - Ancillary

A traversing Pitot-static tube with electronic position measurement for use with TecQuipment’s Subsonic Wind Tunnels (AF1300, AF1450, AF1600).

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