Subsonic Wind Tunnels
![AF1450k 3D Vehicle Models 1122](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1450k-3D-Vehicle-Models.png)
SET OF TWO VEHICLE DRAG MODELS
A generic model van and car to allow students to compare the different coefficient of drag for each vehicle.
![Flutter Wing 0920](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/Flutter-Wing.png)
Flutter Wing
![VDAS](/assets/img/theme/VDAS.png)
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.
![AF1300 1450 1600h Aircraft Models High Wing 0818](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300-1450-1600h-Aircraft-Models-High-Wing.png)
Aircraft Model - High Wing
The high wing model aircraft with NACA profile wings for use with the Large Subsonic Wind Tunnel (AF1600) is good for experiments with lift, drag and pitching moment of fixed wing aircraft.
![Af1600S SUBSONIC WIND TUNNEL 600mm 1118](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/SUBSONIC-WIND-TUNNEL-600mm-AF1600S.jpg)
SUBSONIC WIND TUNNEL 600mm
![VDAS](/assets/img/theme/VDAS.png)
TecQuipment’s largest open-circuit subsonic wind tunnel, with a working section of 600 mm by 600 mm and 1250 mm long, is for the study of advanced aerodynamics theory and research. With the larger size comes greater visualisation and more accurate results, operating at meaningful Reynolds numbers.
![AF1300 1450 1600g Aircraft Models Low Wing 0818](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300-1450-1600g-Aircraft-Models-Low-Wing.png)
Aircraft Model - Low Wing
A low wing model aircraft with NACA2415 profile wings for use with TecQuipment's Large Subsonic Wind Tunnel (AF1600S)
![AF1300_1450_1600j 3D Drag Models 0119](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300_1450_1600j-3D-Drag-Models.png)
Three-Dimensional Drag Models
A set of different shape models with identical frontal area to allow students to compare the different coefficient of drag for each shape. Includes a dummy stem for tests to cancel out the drag due to each model’s support arm.
![AF1300_1450_1600c NACA 2414 Aerofoil with Flap 1018](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300_1450_1600c-NACA-2414-Aerofoil-with-Flap.png)
NACA2412 Aerofoil with Variable Flap
A 150mm chord NACA2412 aerofoil with 590 span featuring a variable flap that adjusts +/- 90 degrees for use with the AF1600 Subsonic Wind Tunnel.
![AF1300_1450_1600b NACA0012 Aerofoil with Tappings 1118](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300_1450_1600b-NACA0012-Aerofoil-with-Tappings.png)
NACA0012 Aerofoil with Tappings
A 150 mm chord NACA0012 aerofoil with 20 static pressure tappings.
![Af1600F 1122](/assets/img/products/Supporting-Products/Specimines/_280x280_fit_center-center_90_none/AF1600f.png)
Flat Plate Boundary Layer Model Roughened and Smooth
A pair of boundary layer models with a mounting plate, also a pitot and a static probe for investigating boundary layer. One plate is roughened, the other smooth to allow comparisons on boundary layer growth.
![AF1300_1450_1600a Cylinder Model](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300_1450_1600a-Cylinder-Model.png)
CYLINDER MODEL
A cylinder model that spans the full width of the working section of the AF1600S Subsonic Wind Tunnel.
![MODULAR AIR FLOW BENCH AF10 0124](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/MODULAR-AIR-FLOW-BENCH-AF10.png.png)
MODULAR AIR FLOW BENCH
This is a small-scale wind tunnel with an electric fan and adjustable air flow control, with eight different experiment modules that demonstrate key principles and phenomena of air flow.
![AF1300 Subsonic Wind Tunnel 1020](/assets/img/products/Aerodynamics/_280x280_fit_center-center_90_none/AF1300-Subsonic-Wind-Tunnel.jpg)
SUBSONIC WIND TUNNEL 305 mm
![VDAS](/assets/img/theme/VDAS.png)
A compact, free-standing, open-circuit suction subsonic wind tunnel with a working section of 305 mm by 305 mm and 600 mm long, allowing students to perform advanced study such as analysing boundary layers, performing flow visualisation and observing velocity in the wake, offering extensive teaching and research functionality.