NASA NTRS · 19780046121
A flow study in radial inflow turbine scroll-nozzle assembly
Abstract
The present analysis describes the flow behavior in the combined scroll-nozzle assembly of a radial inflow turbine. This model was chosen to provide a better understanding of the mutual interaction effects of these two components on the flow. The finite element method is used in the solution of the flow field in this multiply connected domain. The mass flow rates in the different nozzle channels is not presumed constant, but is determined from the solution.
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Hamed, A., Baskharone, E., Tabakoff, W.. 1978-03-01. A flow study in radial inflow turbine scroll-nozzle assembly. https://ntrs.nasa.gov/citations/19780046121
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