An Experimental and Theoretical Investigation of a Twin-Entry Radial Flow Turbine under Non-Steady Flow Conditions University of Manchester, Institute of Science and Technology, (Manchester/England)

Format:

Conference/Event

Author/Creator:

Farrashkhalvat, M., author.

Conference Name:

Aerospace Congress & Exposition (1980-10-13 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1980

Summary:

One of the methods of representing a turbocharger-turbine in the exhaust system of internal combustion engines is by assuming quasi-steady flow at turbine boundaries, while taking into account the generation of pressure waves both upstream and downstream of the turbine due to non-steady flow conditions.This method relies substantially on steady flow turbine characteristics for the generation of boundary conditions. A method is presented to allow for wave action both upstream and downstream of a twin-entry radial inflow turbine. The method also allows for different flow rates in each entry to simulate the partial admission condition. Comparison is made between experimental results and theoretical analysis

Notes:

Vendor supplied data

Publisher Number:

801136

Access Restriction:

Restricted for use by site license