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Cluster Computation of Flight Reynolds Number FlowsThe 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.
Document ID
20010062156
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Atwood, Christopher A.
(NASA Ames Research Center Moffett Field, CA United States)
Smith, Merritt H.
(NASA Ames Research Center Moffett Field, CA United States)
Kutler, Paul
Date Acquired
August 20, 2013
Publication Date
January 1, 1994
Subject Category
Aerodynamics
Meeting Information
Meeting: OAI/NASA Symposium Application of Parallel and Distributed Computing
Location: Columbus, OH
Country: United States
Start Date: April 18, 1994
End Date: April 19, 1994
Sponsors: NASA Headquarters, Ohio Aerospace Inst.
Funding Number(s)
PROJECT: RTOP 509-10-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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