NASA NTRS · 20010062156
Cluster Computation of Flight Reynolds Number Flows
Abstract
The performance of a workstation cluster used for the solution of the Reynolds-averaged Navier-Stokes equations is compared with a conventional vector supercomputer architecture. The application simulation of the steady flowfield about a transonic transport was computed using an implicit diagonal scheme in an overset mesh framework. Static load balancing was used, while coarse grain decomposition was achieved by solution of a grid zone per processor. Price/performance ratios are estimated for several scenarios in which such clusters may be utilized.
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Atwood, Christopher A., Smith, Merritt H., Kutler, Paul. 1994-01-01. Cluster Computation of Flight Reynolds Number Flows. https://ntrs.nasa.gov/citations/20010062156
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