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Propulsion and Heat Transfer Labs


Propulsion lab is equipped with 60 HP Rover Gas Turbine, Two-Shaft Gas Turbine, Axial Flow Compressor, Turbo Fan System and Nozzle Testing Unit. The Heat Transfer Lab houses Free and Forced Convection Apparatus, Radiation Heat Apparatus, Concentric tube heat exchanger, and a Heat Pump. The undergraduate students use most of these for training purposes and for the project work. An Advanced Combustion Lab also forms part of this lab. A Water Turbine demonstration unit, Combustion Demonstration Unit, Thermal conductivity apparatus with steam generator and Flame Reaction Kinetics Unit are other main equipment in this lab.

Propulsion Lab Models1.jpgDSC_0088.jpg