Subsonic Wind Tunnel 450MM Package

Item Number: 
AF1450S - Package
TecQuipment | Aerodynamics Education
Subsonic Wind Tunnel 450MM Package (1450S)
TecQuipment | Aerodynamics Education
Subsonic Wind Tunnel 450MM Package (1450S)
TecQuipment | Aerodynamics Education
Subsonic Wind Tunnel 450MM Package (1450S)
TecQuipment | Aerodynamics Education
Subsonic Wind Tunnel 450MM Package (1450S)
TecQuipment | Aerodynamics Education
Subsonic Wind Tunnel 450MM Package (1450S)
TecQuipment | Aerodynamics Education
TecQuipment | Aerodynamics Education
Subsonic Wind Tunnel 450MM Package (1450S)

A compact, practical open-circuit suction wind tunnel for studying aerodynamics. The wind tunnel saves time and money compared with full-scale wind tunnels or airborne laboratories.

The wind tunnel provides accurate results and is suitable for undergraduate study and research projects.

Air enters the tunnel through an aerodynamically designed effuser (cone) that accelerates the air linearly. It then enters the working section and passes through a grill before moving through a diffuser and then to a variable-speed axial fan. The grill protects the fan from damage by loose objects. The air leaves the fan, passes through a silencer unit and then back out to atmosphere.

A separate control and instrumentation unit controls the speed of the axial fan (and the air velocity in the working section).

A metal frame supports the wind tunnel. The frame includes lockable castors for convenient mobility.

What's Included?Learning OutcomesKey FeaturesAvailable ExperimentsRecommended Ancillaries

Included with the wind tunnel:

  • Three-Component Balance (AF1450T)
  • Balancing Angle Feedback Unit (AFA4)
  • NACA 0012 Aerofoil with Tappings (AF1450B)
  • Dual Differential Pressure Display (DP6)
  • 32-Way Pressure Display Unit (AFA6)
  • Pitot Static Traverse x 2 (AF1450X)
  • Protractor
  • Model Holder
  • Versatile Data Acquisition System (VDAS-F) - frame mounted

Learning Outcomes

A wide variety of subsonic aerodynamics experiments (some need ancillaries), including:

  • Flow past bluff  and streamlined bodies with pressure and velocity observations in the wake
  • Investigations into boundary layer development
  • Influence of aspect ratio on aerofoil performance
  • Performance of an aerofoil with flap, infl uence of flap angle on lift, drag and stall
  • Pressure distribution around a cylinder under sub- and super-critical fl ow conditions
  • Study of characteristics of models involving basic measurement of lift and drag forces
  • Study of the characteristics of three-dimensional aerofoils involving measurements of lift, drag and pitching moment
  • Study of the pressure distribution around an aerofoil model to derive the lift, and comparison with direct measurements of lift
  • Drag force on a bluff  body normal to an air flow
  • Flow visualization

Key Features

  • A cost effective solution when compared to full-scale wind tunnels or airborne laboratories
  • Operates at meaningful Reynolds numbers
  • Safe, open-circuit suction design
  • Package includes an aerofoil with tappings, a three-component balance, angle feedback, dual differential pressure display, a 32-Way pressure display unit, 2 x Pitot static traverse, protractor, model holder and data acquisition (VDAS-F)
  • High levels of safety
  • Controls and instrumentation conveniently mount on a separate, free-standing frame

Available Experiments

CYLINDER MODEL

AF1300A - Experiment

A cylinder model with a single pressure tapping point for use with the AF1300 Subsonic Wind Tunnel.

NACA 2412 AEROFOIL MODEL WITH FLAP

AF1300C - Experiment

A 150 mm chord NACA2412 unsymmetrical section aerofoil with 300 mm span and adjustable flap for use with the AF1300 Subsonic Wind Tunnel.

SET OF 2 NACA 0012 AEROFOIL MODELS

AF1300D - Experiment

A set of two aerofoils both of NACA0012 profile and 150 mm chord for use with the AF1300 Subsonic Wind Tunnel.

FLAT PLATE DRAG MODEL

AF1300E - Experiment

A 100 mm diameter flat plate for use with the AF1300 Subsonic Wind Tunnel.

FLAT PLATE BOUNDARY LAYER MODELL

AF1300F - Experiment

A flat boundary layer model to illustrate the phenomena of boundary layer development and separation. For use with the AF1300 Subsonic Wind Tunnel.

THREE DIMENSIONAL DRAG MODELS

AF1300J - Experiment

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

S1210 AEROFOIL MODEL

AF1300L - Experiment

An S1210 profile aerofoil of 150 mm chord for use with the AF1300 Subsonic Wind Tunnel.

AIRCRAFT MODEL LOW / HIGH WING

AF1300G / AF1300G - Experiment

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

Recommended Ancillaries

MULTI-TUBE MANOMETER

AFA1 - Ancillary

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.

SMOKE GENERATOR

AFA10 - Ancillary

This smoke generator and probe is an optional ancillary to TecQuipment's AF1300 Subsonic Wind Tunnel to allow the observation of airflow in subsonic wind tunnels and other airflow situations.

PITOT STATIC TRAVERSE (DIGITAL)

AFA7 - Ancillary

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

SMOKE GENERATOR

AFA10 - Ancillary

This smoke generator and probe is an optional ancillary to TecQuipment's AF1300 Subsonic Wind Tunnel to allow the observation of airflow in subsonic wind tunnels and other airflow situations.

Recommended Ancillaries

MULTI-TUBE MANOMETER

AFA1 - Ancillary

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.

THREE COMPONENT BALANCE

AF1300T - Ancillary

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

DIFFERENTIAL PRESSURE UNIT

AFA5 - Ancillary

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

32 WAY PRESSURE DISPLAY UNIT

AFA6 - Ancillary

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.

PITOT STATIC TRAVERSE (DIGITAL)

AFA7 - Ancillary

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

SMOKE GENERATOR

AFA10 - Ancillary

This smoke generator and probe is an optional ancillary to TecQuipment's AF1300 Subsonic Wind Tunnel to allow the observation of airflow in subsonic wind tunnels and other airflow situations.

VDAS MKII (FRAME MOUNTED VERSION)

VDAS-F (mkII) - Ancillary

A frame mounting versatile data acquisition system (VDAS) to allow computer-based data capture for a wide range of TecQuipment products.

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