FM-1849-28D Mini Wind Tunnel

Experiments

This wind tunnel supports a wide range of practical experiments to help users understand core aerodynamic principles:

  • Measurement of lift and drag coefficients for different models
  • Investigation of lift and drag variation with angle of attack
  • Study of aerodynamic forces at different air velocities
  • Analysis of drag acting on various shapes and bodies
  • Observation of airflow patterns and streamline behavior using smoke/fog visualization
  • Comparison of aerodynamic performance between different profiles (e.g., aerofoils vs bluff bodies)
  • Effect of airflow uniformity and turbulence on aerodynamic results

Key Features

  • Open-circuit Eiffel-type wind tunnel
  • Transparent test section for clear visualization
  • Flow straightener for reduced turbulence
  • Metal inlet, nozzle, and diffuser for durability
  • Variable-speed fan for adjustable airflow
  • Two-component force sensor for lift and drag measurement
  • Inclined tube manometer for airflow velocity indication
  • Optional DAQ system for computer-based data analysis
  • Compatible with flow visualization accessories

 

FM-1849-28D Mini Wind Tunnel – Educational Aerodynamics System

The FM-1849-28D Mini Wind Tunnel is a compact and efficient laboratory solution designed for practical learning in aerodynamics and fluid mechanics. It allows users to investigate airflow characteristics and evaluate the forces acting on models placed inside a controlled air stream.

This system is based on an open-circuit “Eiffel” type design. Air is drawn from the surroundings, accelerated through a specially shaped inlet and nozzle, and delivered into a transparent test section where experiments are conducted. A built-in flow straightener ensures smooth, low-turbulence airflow, while the diffuser gradually reduces air velocity before discharge.

The unit can generate air velocities up to 20 m/s using an energy-efficient variable-speed fan. Lift and drag forces are measured using a precise two-component force sensor with digital output. Air velocity can be observed through an inclined manometer or optional digital instrumentation.

For enhanced analysis, an optional Data Acquisition (DAQ) system allows real-time monitoring and recording of parameters such as pressure, velocity, angle, and force directly on a computer.

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