NASA NTRS · 19930039283
An efficient nonlinear relaxation technique for the three-dimensional, Reynolds-averaged Navier-Stokes equations
Abstract
An efficient implicit method for the computation of steady, three-dimensional, compressible Navier-Stokes flowfields is presented. A nonlinear iteration strategy based on planar Gauss-Seidel sweeps is used to drive the solution toward a steady state, with approximate factorization errors within a crossflow plane reduced by the application of a quasi-Newton technique. A hybrid discretization approach is employed, with flux-vector splitting utilized in the streamwise direction and central differences with artificial dissipation used for the transverse fluxes. Convergence histories and comparisons with experimental data are presented for several 3-D shock-boundary layer interactions. Both laminar and turbulent cases are considered, with turbulent closure provided by a modification of the Baldwin-Barth one-equation model. For the problems considered (175,000-325,000 mesh points), the algorithm provides steady-state convergence in 900-2000 CPU seconds on a single processor of a Cray Y-MP.
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Edwards, Jack R., Mcrae, D. S.. 1993-01-01. An efficient nonlinear relaxation technique for the three-dimensional, Reynolds-averaged Navier-Stokes equations. https://ntrs.nasa.gov/citations/19930039283
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