Use this URL to cite or link to this record in EThOS: https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.344448
Title: Study of a variable geometry radial inflow turbine
Author: Jasim, Adnan A.
ISNI:       0000 0001 3589 3900
Awarding Body: University of Bath
Current Institution: University of Bath
Date of Award: 1983
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Abstract:
This study is concerned with a variable geometry inward flow radial turbine for turbocharging Diesel engines. A detailed theoretical and experimental investigation in both the stator and rotor is presented. The finite element method being applied for the flow analysis. The finite element procedure was initially developed by applying it to an isolated aerofoil prior to the further application to cover a circular cascade of blades as encountered in the volute-nozzle assembly. In the rotor, only the hub-shroud analysis was carried out and the results compared with an existing streamline curvature technique. It was shown that the finite element method required less computaional time and was more generally applicable to complex geometric configurations than the streamline curvature technique. Experimentally, the turbine performance was evaluated with and without exhaust diffusers and with a number of nozzle rings with different restrictions. It was shown that the maximum restriction resulted in high losses due to the flow mismatching at nozzle inlet because of the sudden area change, and relatively low efficiencies resulted. The effect of swirl, resulting from off-design operation, on the diffusers was analysed with three conical diffusers. The results show that low swirls of the order of 10%, has a beneficial effect on the pressure recovery coefficient for wide angle diffuser.
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID: uk.bl.ethos.344448  DOI: Not available
Keywords: Fluid mechanics
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