Computer Controlled Subsonic Wind Tunnel

To fetch the same or accurate results in different experiments or statistical trials, our products are best proven in all terms. Here we have mentioned the full description, design, specifications regarding all information in a detailed manner.

Product Details:

A wide range of measurements and demonstrations is possible with the equipment. A selection using the models and instrumentation provided are:

• Investigation of the development of the Boundary Layer on a flat plate bymeasurement of the total head distribution
• Flow visualization studies around an aerofoil
• Measurement of pressure distribution around an aerofoil at various anglesof attack
• Measurement of pressure distribution around a cylinder
• Measurement of lift and drag on an aerofoil with leading edge slot and trailingedge flap
• Velocity and pressure distribution measurements using a Pitot static tubeand yaw probe
• Measurement of drag for a selection of models of different shapes but commonequatorial diameter
• Demonstration of flutter of an aerofoil
• Calibration of the Wind Tunnel velocity indicator using a Pitot static tubeand inclined manometer
• Investigation of the wake behind a cylinder or aerofoil using a wake surveyrake

Subsonic Wind Tunnel:

A most simple and safe device is Subsonic Wind Tunnel. To move easily it is mounted on castors. It is a low speed tunnel and operates on very low Mach Number. Ther are different types of this tunnel.

• Open Return Type
• Closed Return Type

Open Return Type: It is based on the principle of  continuity and Bernoulli's equation. Closed wind tunnel: It can reduce the pressure losses and also ensures the smooth flow of test section.