NASA NTRS · 19930036176
The computation of supersonic combustor flows using multi-computers
Abstract
An explicit CFD computer code with parallel processing is developed for the purpose of simulating internal high-speed reacting flows. The code solves the 3D Navier-Stokes equations for compressible flows. Preliminary results indicate that parallel processing should solve the resource and speed shortages presently encountered with sequential computers for problems of interest.
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Underwood, Mark, Riggins, David, Mcmillin, Bruce, Lu, Eric J.-L., Reeves, Larry. 1993-01-01. The computation of supersonic combustor flows using multi-computers. https://ntrs.nasa.gov/citations/19930036176
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