PL- Propulsion Lab Equipments

We are one of the prominent manufacturers and suppliers of the superior quality range of Propulsion lab, which include Free Wall Jet Experiments. The entire range is fabricated using high grade raw materials in compliance with the set industry norms using advanced technology. Our customers can avail this entire range at genuine prices.

Forced/Free convection apparatus – Horizontal

Having capabilities to determining the heat transfer (Qconvection) from a horizontal plate in nature convection over a wide range of power inputs and corresponding surface temperatures.

Measuring the domination of the convective heat transfer coefficient Hc at low surface temperatures and heat transfer coefficient Hr at high surface temperature.

Determining the effect of forced convection on the heat transfer from the plate at varying air velocities.

Consisting of centrifugal fan with vertical outlet duct, K type thermocouples etc.

Forced/Free convection apparatus – Vertical

Having capabilities to determining the heat transfer (Qconvection) from a horizontal plate in nature convection over a wide range of power inputs and corresponding surface temperatures.

Measuring the domination of the convective heat transfer coefficient Hc at low surface temperatures and heat transfer coefficient Hr at high surface temperature.

Determining the effect of forced convection on the heat transfer from the plate at varying air velocities.

Consisting of centrifugal fan with vertical outlet duct, K type thermocouples etc.

Axial compressor blade 3 in number aerofoil model with pressure taping and mechanical operation to be fitted in existing wind tunnel in your lab and water tube manometers (20 tubes) with accessories.

Cascade aerofoil system with manometer – Having capabilities to conduct Drag & lift in horizontal and various angle of attack, pressure distribution in horizontal and various angle of attack. Flow pattern by using smoke generator and to plot different graphs.

For the above test rig, Wind Tunnel is required.

Static and total pressure probes: 2-D traverse in mechanism for 150mm long to your existing Wind tunnel with single ‘U’ tube manometer
	In this instrument the straight line flow of air movement calibration in the wind tunnel can be done.

Nozzle pressure distribution test rig
	To conduct Visual demonstration of choking, pressure distribution. Demonstration of the effect of back pressure on the position of recompression. Determination of the effect of inlet pressure on the mass flow rate with constant back pressure and compare with the theoretical prediction.

Nozzle performance test rig
	To perform Visual Demonstration of choking. Determination of the effect of inlet pressure on mass flow rate given a constant back pressure & comparison with the theoretical predictions. Determination of the effect of back pressure on the mass flow rate. Determination of Jet Velocity and Nozzle efficiency. Determination of Jet reaction and specific thrust.

Free wall jet test setup 1 HP Blower with variable speed drive, X Y Z co-ordinate direction pitot tube and multi bank manometer. Flow distribution tapings on 1mt aluminium platform.

To obtain velocity profile along the length of aluminium plate and velocity profile across the aluminium plate. To conduct experiment on different speeds.

Consisting of blower, motor, velocity measurement, aluminum plate, pitot movement, jet, duct and mounted on sturdy frame of M.S. Angle.

Combustion performance study in RAM / Pulse jet engine along with Combustion chamber.

Continuous combustion unit has been designed to demonstrate handling and operation of typical furnace equipment to students.

A medium pressure liquid-gas burner fires into a stainless steel water-cooled combustion chamber provided with slight glasses and tapping points.

Consisting of burner, observation chamber etc.

Propeller performance test rig

Study of performance of a propeller model test rig to find out thrust by using anemometer, thrust and speed measuring instruments.

Propeller blade angle can be changed upto 10 degree.Motor of 180W capacity, 1500 rpm, and variable speed drive. Having capabilities to fix pitch angle for propeller, perpendicular to axis for maximum efficiency. To measure thrust for different pitch angle and rpm.

Consisting of Aerofoil, motor, blades, velocity measurement, speed measurement, thrust measurement and power measurement.

Blower balance and aspect ratio
	Consisting of Axial type fan, motor, A.C. Drive, aerofoil, digital force indicator, aerofoil angle changing mechanism, anemometer.