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Development of a Navier-Stokes algorithm for parallel-processing supercomputersAn explicit flow solver, applicable to the hierarchy of model equations ranging from Euler to full Navier-Stokes, is combined with several techniques designed to reduce computational expense. The computational domain consists of local grid refinements embedded in a global coarse mesh, where the locations of these refinements are defined by the physics of the flow. Flow characteristics are also used to determine which set of model equations is appropriate for solution in each region, thereby reducing not only the number of grid points at which the solution must be obtained, but also the computational effort required to get that solution. Acceleration to steady-state is achieved by applying multigrid on each of the subgrids, regardless of the particular model equations being solved. Since each of these components is explicit, advantage can readily be taken of the vector- and parallel-processing capabilities of machines such as the Cray X-MP and Cray-2.
Document ID
19890016588
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Swisshelm, Julie M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-102188
NAS 1.15:102188
A-89121
Report Number: NASA-TM-102188
Report Number: NAS 1.15:102188
Report Number: A-89121
Accession Number
89N25959
Funding Number(s)
PROJECT: RTOP 536-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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