SUBSONIC WIND TUNNEL (AF100)

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

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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, and it offers a wide variety of experiments. The wind tunnel gives accurate results and is suitable for undergraduate study and research projects. TecQuipment offers a comprehensive range of optional models and instrumentation, including a computer-based data acquisition system.

AF100 Features

  • Saves time and money compared to full-scale wind-tunnels or airborne laboratories
  • Operates at meaningful Reynolds numbers
  • Compact, open-circuit suction design
  • Wide variety of experiments in aerodynamics
  • Comprehensive selection of optional instrumentation, models and ancillaries
  • High levels of safety
  • Controls and instrumentation conveniently mount on a separate, free standing frame
  • Works with TecQuipment’s Versatile Data Acquisition System (VDAS®) to allow accurate real-time data capture, monitoring and display on a computer

AF100 Experiments

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, influence of flap angle on lift, drag and stall
  • Pressure distribution around a cylinder under sub and super-critical flow conditions
  • Study of characteristics of models involving basic measurement of lift and drag forces
  • Study of the characteristics of three-dimensional aerofoils involving measurement 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 visualisation

AVAILABLE EXPERIMENTS:  The AF100 is a base unit for the following experiment modules and kits

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CYLINDER MODEL (AF101)

A cylinder model with a single pressure tapping point for use with the AF100 Subsonic Wind Tunnel.

NACA 0012 AEROFOIL WITH TAPPINGS (AF102)

A 150 mm chord 300 mm span NACA0012 aerofoil with pressure tappings for use with the AF100 Subsonic Wind Tunnel.

NACA 2412 AEROFOIL WITH FLAP (AF103)

A 150 mm chord NACA2412 unsymmetrical section aerofoil with 300 mm span and adjustable flap for use with the AF100 Subsonic Wind Tunnel.

SET OF 2 NACA 0012 AEROFOILS (AF104)

A set of two aerofoils both of NACA0012 profile and 150 mm chord for use with the AF100 Subsonic Wind Tunnel.

ALTERNATIVES:  Products with similar functionality to the AF100

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MODULAR AIR FLOW BENCH (AF10)

A fully mobile bench to provide basic airflow facilities to enable a wide range of practical airflow investigations. Suitable for demonstration, laboratory and project work at a basic level.

FLIGHT DEMONSTRATION WIND TUNNEL (AF41)

An open-circuit wind tunnel incorporating a suspended aircraft model with realistic controls for classroom demonstrations and student investigations into a variety of aircraft flight principles.

FLOW VISUALISATION WIND TUNNEL (AF80)

A floor standing suction type subsonic wind tunnel with smoke visualisation that allows demonstrations and student investigations into the flow of air around a wide variety of different shaped models.

SUPERSONIC WIND TUNNEL (INTERMITTENT) (AF300)

The AF300 is an intermittent operation induction type supersonic wind tunnel that allows investigations into the flow around 2-dimensional models at supersonic airspeeds.

Works with
VDAS Logo
Click here for details.