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Performance of a parallel code for the Euler equations on hypercube computersThe performance of hypercubes were evaluated on a computational fluid dynamics problem and the parallel environment issues were considered that must be addressed, such as algorithm changes, implementation choices, programming effort, and programming environment. The evaluation focuses on a widely used fluid dynamics code, FLO52, which solves the two dimensional steady Euler equations describing flow around the airfoil. The code development experience is described, including interacting with the operating system, utilizing the message-passing communication system, and code modifications necessary to increase parallel efficiency. Results from two hypercube parallel computers (a 16-node iPSC/2, and a 512-node NCUBE/ten) are discussed and compared. In addition, a mathematical model of the execution time was developed as a function of several machine and algorithm parameters. This model accurately predicts the actual run times obtained and is used to explore the performance of the code in interesting but yet physically realizable regions of the parameter space. Based on this model, predictions about future hypercubes are made.
Document ID
19910002071
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Barszcz, Eric
(California Univ. Los Angeles., United States)
Chan, Tony F.
(NASA Ames Research Center Moffett Field, CA, United States)
Jesperson, Dennis C.
(NASA Ames Research Center Moffett Field, CA, United States)
Tuminaro, Raymond S.
(Stanford Univ. CA., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Mathematical And Computer Sciences (General)
Report/Patent Number
A-90020
NAS 1.15:102260
NASA-TM-102260
Report Number: A-90020
Report Number: NAS 1.15:102260
Report Number: NASA-TM-102260
Accession Number
91N11384
Funding Number(s)
PROJECT: RTOP 536-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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