The Drag Forces Module | FluidoSurge-X 352 by SCIENTICO is an experimental accessory for measuring drag forces and determining drag coefficients on plates, cylinders, and aerofoils. It includes a beam scale and adjustable Pitot tube for pressure and wake analysis. Designed for use with the compatible aerodynamics trainer in fluid mechanics laboratories.
The Drag Forces Module FluidoSurge-X 352 is a laboratory accessory designed for experimental determination of drag forces and drag coefficients on bodies immersed in airflow. Manufactured by SCIENTICO, the unit enables quantitative analysis of flow-induced forces and wake behavior in aerodynamic studies. It is intended for use with the compatible Aerodynamics Trainer.
Product Overview
FluidoSurge-X 352 allows measurement of drag forces acting on different body shapes such as flat plates, cylinders, and aerofoil models. The forces generated by airflow are measured using a beam scale with movable weight. A Pitot tube system enables recording of pressure distribution and velocity profiles downstream of the test body. The module supports experimental investigation of wake depression and flow behavior around bluff and streamlined bodies. The unit attaches to the compatible aerodynamics trainer using quick release fasteners for secure and accurate positioning.
Measuring Section
| Parameter | Specification |
|---|---|
| Cross Section | 50 x 100 mm |
| Angle Scale | ±35 degrees |
Pitot Tube
| Parameter | Specification |
|---|---|
| Diameter | 1.2 mm |
| Horizontal Adjustment | ±50 mm |
Drag Bodies
| Model | Dimensions |
|---|---|
| Plate | 45 x 15 x 10 mm |
| Cylinder | Diameter 25 mm x Height 75 mm |
| Aerofoil Model | 100 x 15 x 40 mm |
Key Features
-
Measurement of drag forces on different body shapes
-
Determination of drag coefficients
-
Beam scale with movable weight for force measurement
-
Pitot tube for pressure and velocity profile measurement
-
Wake depression analysis downstream of cylinder
-
Quick release attachment to compatible aerodynamics trainer
-
Modular design for laboratory flexibility
Applications
-
Fluid mechanics and aerodynamics laboratories
-
Study of drag forces and aerodynamic coefficients
-
Pressure distribution measurement around bluff bodies
-
Wake analysis and velocity profile measurement
-
Engineering education in vehicle and structural aerodynamics
Construction & Design Details
The module consists of a measuring section fitted with interchangeable drag bodies. A beam scale arrangement measures flow-induced forces directly. The Pitot tube can be adjusted horizontally and inclined relative to the flow direction to record total pressures and determine downstream velocity profiles. The cylinder model includes an additional pressure measuring point for detailed pressure distribution analysis.
Experiments
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Measurement of drag forces on immersed bodies
-
Determination of drag coefficients
-
Indirect drag measurement using pulse rate
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Recording pressure distribution on a cylinder
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Measurement of wake depression behind a cylinder
-
Determination of downstream velocity profile
Optional Accessories
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Multitude manometers
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Aerofoil with tapping points for pressure measurement
Required for Operation
-
Aerodynamics Trainer FluidoSurge-X 352 (sold separately)
Standard Scope of Delivery
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1 Experimental Module
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1 Set of Drag Bodies
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1 Pitot Tube
-
1 Instruction Manual
Export & Supply Capability
SCIENTICO manufactures the Drag Forces Module FluidoSurge-X 352 for engineering institutions and research laboratories. The unit is suitable for domestic and international supply, with export packing and documentation provided as required.
Q1. What bodies are included for drag measurement?
The module includes a flat plate, a cylinder, and an aerofoil model.
Q2. How are drag forces measured?
Drag forces are measured using a beam scale with movable weight.
Q3. Can pressure distribution be measured?
Yes. A Pitot tube is used to record pressure distribution and velocity profiles.
Q4. Is the module standalone?
No. It requires a compatible aerodynamics trainer for operation.
Q5. What additional studies can be performed?
Wake depression and velocity profile downstream of a cylinder can be investigated.
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