Subsonic Wind Tunnel Lab Equipment Manufacturer, Supplier and Exporter in India

Catalogue No : EE-0825

Subsonic Wind Tunnel The setup is an open breeze burrow used to exhibit and measure the streamlined properties of different models. For this reason, air is attracted from the earth and quickened. The wind currents around a model, for example, an aerofoil, in an estimating segment. The air is then decelerated in a diffuser and pumped over beyond any confining influence by a fan. The deliberately outlined admission spout and a stream straightener guarantee a uniform speed appropriation with little turbulence in the shut estimating area. The test area is square fit as a fiddle & made of tranparent plexiglass for understudies to imagine the procedure. The inherent pivotal fan with a variable-speed drive is portrayed by a vitality productive task at high effectiveness. Air speeds of up to 36 m/s are conceivable to be accomplished in the breeze burrow. The mentor is outfitted with an electronic two-segment constrain sensor. Lift and drag are recognized and shown carefully. The air speed in the test segment is estimated utilizing a pitor tube. The standard embellishments incorporate Multitube Inclined Manometer, Static Pitot Tube, U tube Manometer, 2 Component Force Balance, Digital Force Indicator, Wide scope of test modules like NACA aerofoils, drag models of diffrent shapes, Boundry Layer, Airplane Models and so forth are accessible for use with wind burrow & can be requested seperately.An discretionary Data Acquisition System is likewise accessible for perusing estimations of weight, dislodging/point, speed and power. These parameters can be exchanged to a PC where they can be investigated with a windows based software.Optional frill permit an assortment of examinations, for instance lift estimations, point estimation, weight dispersions, limit layer investigation or perception of streamlines. Trial Capabilities: • Determine drag and lift coefficients for various models • Pressure circulation when streaming around drag bodies • Boundary layer examination • Investigation of vacillate • Wake estimation • Visualization of streamlines Standard Accessories: • Multi-Tube Manometer • U tube Manometer • Basic Lift and Drag Balance • Digital Force Indicator Experimental Modules: • Cylinder Model with Pressure Tapping • 150 mm Chord NACA0012 Aerofoil with Tappings • 150 mm Chord NACA2412 Aerofoil with Variable Flap • 150 mm Chord NACA0012 Aerofoils • 100 mm Flat Plate • Flat Boundary Layer Model • Aircraft Model - Low Wind • Aircraft Model - High Wing • Three Dimensional Drag Models Optional Accessories: • Versatile Data Acquisition System • Differential Pressure Indicator • Basic Lift and Drag Balance • Three-Component Balance • Angle Feedback Unit • Differential Pressure Transducer • 32-Way Pressure Display Unit • Pitot-Static Traverse (300 mm) • Smoke Generator.

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