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Simulation of Multistage Turbine FlowsThe numerical simulation of turbine flows serves to enhance the understanding of the flow phenomena within multistage turbomachinery components. The direct benefit of this activity is improved modeling capability, which can be used to improve component efficiency and durability. A hierarchy of equations was formulated to assess the difficulty in analyzing the flow field within multistage turbomachinery components. The Navier-Stokes equations provides the most complete description. The simplest description is given by a set of equations that govern the quasi-one-dimensional flow. The number of unknowns to be solved for increases monotonically above the number of equations. The development of the additional set of equations needed to mathematically close the system of equations forms the closure problem associated with that level of description. For the Navier-Stokes equation there is no closure problem. For the quasi-one-dimensional equation set random flow fluctuations, unsteady fluctuations, nonaxisymmetric flow variations, and hub-to-shroud variations on the quasi-one-dimensional flow must be accounted for.
Document ID
19850019633
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Celestina, M. L.
(Sverdrup Technology, Inc., Middleburg Heights Ohio, United States)
Mulac, R. A.
(Sverdrup Technology, Inc., Middleburg Heights Ohio, United States)
Adamczyk, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1985
Publication Information
Publication: Struct. Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
85N27945
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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