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Saini science industries manufacture of WIND TUNNEL TEST RIG.
“WIND TUNNEL” has been developed to perform various experiments of aerodynamics and fluid flow. This is a open circuit Wind Tunnel provides a region of controlled air flow into which models can be fitted at downstream of working section. The Tunnel consists of bell mouth shaped entry to guide the air smoothly into settling chamber and stabilizes the air flow this follows working section for test section where various models can be tested. Test section with acrylic sheet, will be provided for visual observation. Working section is followed by diffuser section which reduces the dynamic pressure at the exit. A fan coupled with motor is used to produce desired wind velocity.
To plot speed curve for wind tunnel.
Determine drag and lift coefficients for different models
Pressure distribution when flowing around drag bodies
Boundary layer analysis
Investigation of flutter
Required for Operation:
Electricity Supply : 3 Phase, 440V AC, 3 KW
Floor Area: 5.0 x 3.5 m
Variable Speed : 3HP motor with Speed Controller
Type : Open Type Wind Tunnel.
Test Section : 300 x 300 x 1000 mm.
Blower : Compatible Capacity
Air Velocity : Maximum 30 m/s (in Test Section).
Digital Force Indicator : For Lift and Drag force
Multiple Manometer : 0-40° inclination with vertical axis.
U Tube Manometer : Length 500 mm.
Inclined manometer : 300 mm (For cylinder)
Pitot Static Tube : For Velocity Measurement
Micro-Pitot Tube : For Boundary Layer Experiment
An ENGLIThe whole set-up is ingeniously designed and schematically arranged on a powder-coated rigid structure
Standard make On/Off switch, Mains Indicator etc.
MCB : for over load protection.
Scope of Delivery:
Self Contained “WIND TUNNEL TEST RIG.”Apparatus
Instruction Manual consisting of experimental procedures, block diagram etc.