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Comparison of Full and Partial Admission Flow Fields in the Simplex TurbineThis viewgraph presentation provides information on computerized simulations of flow fields in a Simplex turbine. The motivations for the simulation were: Determining the effects of partial admission flow on rotor performance as a function of circumferential location and on unsteady rotor loading; Providing an efficient technique for determining turbine performance. The simulation used the flow code CORSAIR.
Document ID
20030000731
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Dorney, Daniel J. (NASA Marshall Space Flight Center Huntsville, AL United States)
Griffin, Lisa W. (NASA Marshall Space Flight Center Huntsville, AL United States)
Sondak, Douglas L. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 21, 2013
Publication Date
July 1, 2002
Publication Information
Publication: Twelfth Thermal and Fluids Analysis Workshop
Subject Category
Fluid Mechanics And Thermodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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