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An Experimental and Computational Study of Pulsating Flow within a Double Entry Turbine with Different Nozzle Settings
2015
This thesis presents a detailed study of the performance of a nozzled, double entry turbine. This configuration is primarily found in the turbocharger application and encompasses two different entries, each feeding 180° of a single turbine wheel. The primary motives for this research are to enhance the knowledge and understanding of the behaviour of such a device under steady and pulsating flows including the effect of three different nozzle vane geometries. The work incorporates both
doi:10.25560/23909
fatcat:tyes3iixgrb6fnppulwsf7sgiy