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Implicit/Multigrid Algorithms for Incompressible Turbulent Flows on Unstructured GridsAn implicit code for computing inviscid and viscous incompressible flows on unstructured grids is described. The foundation of the code is a backward Euler time discretization for which the linear system is approximately solved at each time step with either a point implicit method or a preconditioned Generalized Minimal Residual (GMRES) technique. For the GMRES calculations, several techniques are investigated for forming the matrix-vector product. Convergence acceleration is achieved through a multigrid scheme that uses non-nested coarse grids that are generated using a technique described in the present paper. Convergence characteristics are investigated and results are compared with an exact solution for the inviscid flow over a four-element airfoil. Viscous results, which are compared with experimental data, include the turbulent flow over a NACA 4412 airfoil, a three-element airfoil for which Mach number effects are investigated, and three-dimensional flow over a wing with a partial-span flap.
Document ID
20040110438
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Anderson, W. Kyle
(NASA Langley Research Center Hampton, VA, United States)
Rausch, Russ D.
(National Academy of Sciences - National Research Council Hampton, VA, United States)
Bonhaus, Daryl L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1997
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 95-1740
Distribution Limits
Public
Copyright
Public Use Permitted.
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