A model aircraft with high wing configuration for use in TecQuipment's AF1300 Wind Tunnel.
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.
AF1300S - Package
A starter set consisting of the Subsonic Wind Tunnel 305 mm (AF1300), Basic Lift and Drag Balance (AF1300z) and a set of Three-Dimensional Drag Models (AF1300j).
Supports wind tunnel models in the AF1300 Subsonic Tunnel and measures their lift, drag and pitching moment.
Compact instrument that fixes to the Three Component Balance (AF1300T). It measures the angle positions of models mounted in the balance and feeds the information directly to the Versatile Data Acquisition System (VDAS®).
Digital differential pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnel (AF1300).
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.
A model aircraft with low wing configuration for use in TecQuipment's AF1300 Wind Tunnel.