NASA NTRS · 19890002945
Three-dimensional multigrid algorithms for the flux-split Euler equations
Abstract
The Full Approximation Scheme (FAS) multigrid method is applied to several implicit flux-split algorithms for solving the three-dimensional Euler equations in a body fitted coordinate system. Each of the splitting algorithms uses a variation of approximate factorization and is implemented in a finite volume formulation. The algorithms are all vectorizable with little or no scalar computation required. The flux vectors are split into upwind components using both the splittings of Steger-Warming and Van Leer. The stability and smoothing rate of each of the schemes are examined using a Fourier analysis of the complete system of equations. Results are presented for three-dimensional subsonic, transonic, and supersonic flows which demonstrate substantially improved convergence rates with the multigrid algorithm. The influence of using both a V-cycle and a W-cycle on the convergence is examined.
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Anderson, W. Kyle, Thomas, James L., Whitfield, David L.. 1988-11-01. Three-dimensional multigrid algorithms for the flux-split Euler equations. https://ntrs.nasa.gov/citations/19890002945
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