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An implicit numerical scheme for the simulation of internal viscous flows on unstructured gridsThe Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows. The grids are generated based on the method of Delaunay triangulation. A finite-volume approach is used to discretize the conservation law form of the compressible flow equations written in terms of primitive variables. A preconditioning matrix is added to the equations so that low Mach number flows can be solved economically. The equations are time marched using either an implicit Gauss-Seidel iterative procedure or a solver based on a conjugate gradient like method. A four color scheme is employed to vectorize the block Gauss-Seidel relaxation procedure. This increases the memory requirements minimally and decreases the computer time spent solving the resulting system of equations substantially. A factor of 7.6 speed up in the matrix solver is typical for the viscous equations. Numerical results are obtained for inviscid flow over a bump in a channel at subsonic and transonic conditions for validation with structured solvers. Viscous results are computed for developing flow in a channel, a symmetric sudden expansion, periodic tandem cylinders in a cross-flow, and a four-port valve. Comparisons are made with available results obtained by other investigators.
Document ID
19940019081
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jorgenson, Philip C. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Pletcher, Richard H.
(Iowa State Univ. of Science and Technology, Ames., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Numerical Analysis
Report/Patent Number
NASA-TM-106437
NAS 1.15:106437
AIAA PAPER 94-0306
E-8279
ICOMP-93-48
Report Number: NASA-TM-106437
Report Number: NAS 1.15:106437
Report Number: AIAA PAPER 94-0306
Report Number: E-8279
Report Number: ICOMP-93-48
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: AIAA
Accession Number
94N23554
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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