NASA NTRS · 19890029658
An implicit flux-split algorithm for the compressible Navier-Stokes equations
Abstract
An implicit upwind scheme for the compressible Navier-Stokes equations is described and applied to the internal flow in a dual-throat nozzle. The method is second-order accurate spatially and naturally dissipative. A spatially-split approximate factorization method is used to obtain efficient steady-state solutions on the NASA Langley VPS-32 (CYBER 205) supercomputer.
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Thomas, James L., Rumsey, Christopher L., Walters, Robert W., Van Leer, Bram. 1987-01-01. An implicit flux-split algorithm for the compressible Navier-Stokes equations. https://ntrs.nasa.gov/citations/19890029658
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