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Nonlinear Fluid Computations in a Distributed EnvironmentThe performance of a loosely and tightly-coupled workstation cluster is compared against a conventional vector supercomputer for the solution the Reynolds- averaged Navier-Stokes equations. The application geometries include a transonic airfoil, a tiltrotor wing/fuselage, and a wing/body/empennage/nacelle transport. Decomposition is of the manager-worker type, with solution of one grid zone per worker process coupled using the PVM message passing library. Task allocation is determined by grid size and processor speed, subject to available memory penalties. Each fluid zone is computed using an implicit diagonal scheme in an overset mesh framework, while relative body motion is accomplished using an additional worker process to re-establish grid communication.
Document ID
19960020488
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)
Date Acquired
September 6, 2013
Publication Date
January 12, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:200825
NASA-CR-200825
AIAA Paper 95-0224
Report Number: NAS 1.26:200825
Report Number: NASA-CR-200825
Report Number: AIAA Paper 95-0224
Meeting Information
Meeting: AIAA 33rd Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 9, 1995
End Date: January 12, 1995
Accession Number
96N24059
Funding Number(s)
CONTRACT_GRANT: NCC2-799
Distribution Limits
Public
Copyright
Public Use Permitted.
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