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A flow study in radial inflow turbine scroll-nozzle assemblyThe 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.
Document ID
19780046121
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hamed, A. (Cincinnati Univ. OH, United States)
Baskharone, E. (Cincinnati Univ. OH, United States)
Tabakoff, W. (Cincinnati, University Cincinnati, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
ASME PAPER 77-WA/FE-4
Accession Number
78A30030
Funding Number(s)
CONTRACT_GRANT: NSG-3066
Distribution Limits
Public
Copyright
Other

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