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- W2044497367 abstract "This work was focused on the development of models for turbomachinery unsteady performance that could capture the significant aspects of fluid inertia effects, and thus provide insight into performance in highly unsteady flows. The application chosen for this approach was the turbine from a pulse-turbocharged diesel engine turbocharger, where the flow unsteadiness in on the order of the mean flow. The Euler Equation with Source Terms (EEST) technique was employed, with the rotor modeled in the relative reference frame. The results of this approach showed the ability to accurately predict the dynamics of a twin-entry turbine operating in an on-engine environment. In general, the modeling approach is valid for any compression or expansion system where the reduced frequency is high enough to suggest that unsteadiness is important, while at the same time low enough that that viscous effects may be quasi-steady. Possible applications would be predictions for aircraft engine compressions systems with unsteady inlet distortions, start up transients in a broad class of turbomachines, and any radial flow systems operating with significant inlet or exit volute generated distortions." @default.
- W2044497367 created "2016-06-24" @default.
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- W2044497367 date "2001-06-04" @default.
- W2044497367 modified "2023-09-23" @default.
- W2044497367 title "A Model for Radial Flow Turbine Performance in Highly Unsteady Flows" @default.
- W2044497367 doi "https://doi.org/10.1115/2001-gt-0312" @default.
- W2044497367 hasPublicationYear "2001" @default.
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