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Development of an explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbo-machineryA rapid quasi three-dimensional analysis was developed for blade-to-blade flows in turbomachinery. The analysis solves the unsteady Euler or thin layer Navier-Stokes equations in a body-fitted coordinate system. It accounts for the effects of rotation, radius change, and stream-surface thickness. The Baldwin-Lomax eddy-viscosity model is used for turbulent flows. The equations which are solved by a two-stage Runge-Kutta scheme made efficient by use of vectorization, a variable time-step, and a flux-based multigrid scheme, are described. A stability analysis is presented for the two-stage scheme. Results for a flat-plate model problem show the applicability of the method to axial, radial, and rotating geometries. Results for a centrifugal impeller and a radial diffuser show that the quasi three-dimensional viscous analysis can be a practical design tool.
Document ID
19860001679
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chima, R. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TM-87128
NAS 1.15:87128
E-2681
Report Number: NASA-TM-87128
Report Number: NAS 1.15:87128
Report Number: E-2681
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: Reno, Nevada
Start Date: January 6, 1986
End Date: January 9, 1986
Sponsors: AIAA
Accession Number
86N11146
Funding Number(s)
PROJECT: RTOP 505-31-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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