The Wind Tunnel FluidoSurge-X 216 is an Eiffel type subsonic wind tunnel for aerodynamic experiments. It enables measurement of lift, drag, velocity, and pressure distribution on models. The setup includes a transparent measuring section, force sensor, and multi tube manometer. It is suitable for aerodynamics and fluid mechanics laboratory teaching.
The Wind Tunnel FluidoSurge-X 216 is designed for experimental study of aerodynamic flow and force characteristics on bodies in air. It enables controlled investigation of lift, drag, pressure distribution, and boundary layer behavior. The system uses an Eiffel type open circuit configuration with a transparent measuring section. It is suitable for aerodynamics and fluid mechanics laboratory instruction.
Product Overview
The SCIENTICO Wind Tunnel FluidoSurge-X 216 is an experimental subsonic wind tunnel used to demonstrate aerodynamic principles under controlled airflow conditions. Air is drawn from the environment, accelerated through a nozzle, and guided through a closed transparent measuring section where models remain stationary. A diffuser decelerates the flow before it is discharged back to the atmosphere by an axial fan. Uniform velocity distribution with minimal turbulence is achieved using a carefully designed inlet contour, nozzle, and flow straightener. The system is equipped with an electronic two component force sensor for direct measurement of lift and drag. Air velocity is indicated using an inclined tube manometer and digital display. A sixteen tube manometer is provided for detailed pressure distribution measurements on test models.
| Parameter | Specification |
|---|---|
| Model | FluidoSurge-X 216 |
| Type | Subsonic Wind Tunnel |
| Configuration | Eiffel type, open circuit |
| Measuring Section Size | 300 x 300 mm |
| Measuring Section Length | 450 mm |
| Wind Velocity Range | 0 to 30 m per second |
| Axial Fan Speed | 0 to 2800 rpm |
| Fan Power Consumption | 2.55 kW |
| Maximum Air Flow | 2.5 m³ per second |
| Fan Head | 500 Pa |
| Force Measurement Range | 2 units, -5 to 5 N |
| Force Resolution | 0.001 N |
| Pressure Measurement Range | 0 to 5 mbar |
| Pressure Resolution | 0.1 Pa |
Key Features-
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Eiffel type open circuit subsonic wind tunnel
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Transparent closed measuring section for observation
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Uniform airflow with reduced turbulence
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Electronic two component force sensor for lift and drag
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Digital display of velocity, angle, lift, and drag
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Sixteen tube water manometer for pressure distribution
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Variable speed axial fan for energy efficient operation
Applications-
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Determination of lift and drag coefficients
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Pressure distribution on aerofoils and drag bodies
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Boundary layer analysis and wake measurement
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Study of flutter and aerodynamic instability
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Visualization of streamlines using smoke generator
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Aerodynamics and fluid mechanics laboratory experiments
Construction & Design Details-
The wind tunnel features a metal inlet contour, nozzle, and diffuser to ensure stable airflow. A flow straightener minimizes turbulence in the measuring section. The measuring section is transparent to allow clear visualization of models and flow behavior. The axial fan includes guide vanes and variable speed control for precise airflow adjustment. Instrumentation includes digital displays, inclined manometer, and a multi angle sixteen tube manometer.
Standard Supplied Models and Accessories-
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Sphere
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Hemisphere
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Circular disc
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Circular ring
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Square plate
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Flag
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Cylinder
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Streamlined shape
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Aerofoil NACA 15
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Paraboloid
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Concave shape
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Boundary layer plate
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Smooth and rough plates
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Pitot tube probe with micrometer
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Smoke generator
Optional Software-
Optional data acquisition software FluidoSurge-X 216 is available.
The software is developed in a LabVIEW™ environment and provides a comprehensive solution for:
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Data acquisition of pressure, velocity, angle, lift, and drag
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Data processing and graphical visualization
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Tabular presentation of measured and calculated values
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Generation of CSV reports including graphs
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Operation on Windows based systems
Electronic sensors required for software operation are supplied when the software option is selected.
Export & Supply Capability-
SCIENTICO manufactures the Wind Tunnel FluidoSurge-X 216 for domestic and international supply. The system is suitable for export to engineering colleges, universities, and aerospace training institutes. Standard packing, accessories, and technical documentation are provided with each unit.
Q1. What type of wind tunnel is this system?
It is an Eiffel type open circuit subsonic wind tunnel.
Q2. What maximum air velocity can be achieved?
Air velocities up to 30 m per second can be reached.
Q3. Can lift and drag be measured directly?
Yes, an electronic two component force sensor measures lift and drag directly.
Q4. Is pressure distribution measurement possible?
Yes, a sixteen tube water manometer is provided for pressure distribution studies.
Q5. Is data acquisition software included as standard?
No, the FluidoSurge-X 216 software is optional and supplied only when specified.
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Flow rates are determined using lever based weights or optional digital load cells.
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An integrated flume supports weir experiments, while the GRP construction ensures long-term laboratory use.
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