The Bernoulli’s Principle Module | FluidoSurge-X 358 by SCIENTICO is a Venturi-based laboratory accessory for demonstrating the continuity equation and Bernoulli’s principle. It enables measurement of static, total, and dynamic pressures using a Pitot-static tube and manometer system. Designed for use with the Aerodynamics Trainer FluidoSurge-X 348.
Mini Wind Tunnel | FluidoSurgeX 219
The Mini Wind Tunnel | FluidoSurgeX 219 by SCIENTICO is an Eiffel type subsonic wind tunnel for aerodynamics and fluid mechanics laboratories. It enables measurement of lift, drag, velocity, and angle of attack on stationary models. The system features a transparent measuring section, low-turbulence airflow, and electronic force measurement. Optional DAQ hardware and software support digital data acquisition and reporting. Suitable for academic teaching and laboratory experimentation.
The Mini Wind Tunnel FluidoSurgeX 219 is a laboratory-scale subsonic wind tunnel designed for aerodynamics and fluid mechanics experiments. Manufactured by SCIENTICO, it enables controlled study of airflow behavior around stationary test models. The system supports accurate measurement of lift, drag, velocity, and angle of attack. Optional digital data acquisition enhances experimental analysis.
Product Overview
FluidoSurgeX 219 is an Eiffel type open-circuit wind tunnel in which air is drawn in, accelerated through a nozzle, and directed through a transparent measuring section. Test models such as aerofoils and drag bodies are mounted within this section for observation and force measurement. After passing the model, air decelerates in a diffuser and is expelled back into the atmosphere by a fan. Flow straighteners and inlet contour ensure uniform, low-turbulence airflow suitable for educational and laboratory use.
| Parameter | Specification |
|---|---|
| Wind Tunnel Type | Eiffel type open system |
| Measuring Section Cross Section (W x H) | 125 × 125 mm |
| Measuring Section Length | 145 mm |
| Wind Velocity Range | 0 to 20 m/s |
| Fan Head | 350 Pa |
| Fan Speed | 0 to 2800 rpm |
| Power Consumption | 0.37 kW |
| Force Measuring Range | 2 × -5 to 5 N |
| Force Resolution | 0.001 N |
| Angle of Attack Range | -90° to +90° |
| Angle Resolution | 1° |
| Velocity Measurement | Inclined tube manometer |
| Force Measurement | Electronic two-component force sensor |
| Data Acquisition System | Optional |
| Software | Optional FM-1849-28DSW |
Key Features-
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Eiffel type wind tunnel for aerodynamics and fluid mechanics experiments
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Transparent, closed measuring section for clear flow observation
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Metal inlet contour, nozzle, and diffuser for stable airflow
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Flow straightener to reduce turbulence
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Variable-speed fan motor for energy-efficient operation
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Digital display of lift and drag forces
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Manual or digital angle of attack adjustment with DAQ option
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Compatible with optional smoke generator for streamline visualization
Applications-
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Aerodynamics laboratory experiments
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Fluid mechanics teaching and demonstrations
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Determination of lift and drag coefficients
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Study of drag on different body shapes
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Streamline visualization using smoke or fog systems
Construction & Design Details-
The wind tunnel incorporates metal construction for the inlet contour, nozzle, and diffuser to ensure stable airflow characteristics. The measuring section is transparent, allowing visual inspection of airflow and interaction with test models. Aerodynamic forces are measured using an electronic two-component force sensor, while air velocity is indicated via an inclined tube manometer. Angle of attack can be adjusted manually or digitally when the DAQ system is used.
Data Acquisition Software (Optional)-
The optional DAQ software is designed for use with the FluidoSurgeX 219 when equipped with the data acquisition system. Developed in the NITM LabVIEW™ environment, the software enables real-time acquisition, processing, and visualization of experimental data on a Windows-based PC.
Measured parameters such as pressure, air velocity, angle of attack, and aerodynamic forces are displayed numerically and graphically. The software allows aggregation of measured and calculated values into tables, plots, and images. At the end of each experiment, a comprehensive CSV report containing all recorded data and graphs can be generated for documentation and further analysis.
Experiments-
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Determination of lift and drag coefficients for different models
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Study of lift and drag at varying angles of attack
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Study of lift and drag at different air velocities
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Drag measurement on different body shapes
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Streamline visualization in conjunction with an optional smoke generator
Standard Scope of Delivery-
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1 experiment module
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1 set of drag bodies
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Inclined tube manometer
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Instruction manual
Export & Supply Capability-
SCIENTICO manufactures the FluidoSurgeX 219 for supply to engineering colleges, technical universities, and research laboratories. The equipment is suitable for domestic and international shipments. Export packaging, documentation, and accessory configurations are provided as per customer and destination requirements.
Q1. What type of wind tunnel is FluidoSurgeX 219?
It is an Eiffel type open-circuit subsonic wind tunnel.
Q2. What is the maximum wind speed achievable?
The system can generate air velocities up to 20 m/s.
Q3. Is the data acquisition system included as standard?
No. The DAQ system and software are available as optional accessories.
Q4. What parameters can be measured using this wind tunnel?
Lift, drag, air velocity, pressure, and angle of attack can be measured.
Q5. Can airflow visualization be performed?
Yes. Streamline visualization is possible using an optional smoke or fog generator.
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An integrated flume supports weir experiments, while the GRP construction ensures long-term laboratory use.
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