Search NASA⌕ Search

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.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Atwood, Christopher A., Smith, Merritt H., Kutler, Paul. 1994-01-01. Cluster Computation of Flight Reynolds Number Flows. https://ntrs.nasa.gov/citations/20010062156

Cite the original work for its findings. Save a collection to share your selection of sources.