A CE-certified aerodynamics laboratory unit for flow visualisation, boundary layer studies, and lift/drag measurement, manufactured by Scientico India to ISO 9001:2015 standards. Supplied with calibration certificate, operation manual, and complete export documentation. Designed for Fluid Mechanics laboratories in engineering colleges and technical institutions.

| 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-
Eiffel type wind tunnel for aerodynamics and fluid mechanics experiments
Transparent, closed measuring section for clear flow observation
Metal inlet contour, nozzle, and diffuser for stable airflow
Flow straightener to reduce turbulence
Variable-speed fan motor for energy-efficient operation
Digital display of lift and drag forces
Manual or digital angle of attack adjustment with DAQ option
Compatible with optional smoke generator for streamline visualization
Applications-
Aerodynamics laboratory experiments
Fluid mechanics teaching and demonstrations
Determination of lift and drag coefficients
Study of drag on different body shapes
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-
Determination of lift and drag coefficients for different models
Study of lift and drag at varying angles of attack
Study of lift and drag at different air velocities
Drag measurement on different body shapes
Streamline visualization in conjunction with an optional smoke generator
Standard Scope of Delivery-
1 experiment module
1 set of drag bodies
Inclined tube manometer
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.
Recommended Accessories (optional)
Smoke Generator
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.