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Vectorizable implicit algorithms for the flux-difference split, three-dimensional Navier-Stokes equationsThe computational efficiency of four vectorizable implicit algorithms is assessed when applied to calculate steady-state solutions to the three-dimensional, incompressible Navier-Stokes equations in general coordinates. Two of these algorithms are characterized as hybrid schemes; that is, they combine some approximate factorization in two coordinate directions with relaxation in the remaining spatial direction. The other two algorithms utilize an approximate factorization approach which yields two-factor algorithms for three-dimensional systems. All four algorithms are implemented in identical high-resolution upwind schemes for the flux-difference split Navier-Stokes equations. These highly nonlinear schemes are obtained by extending an implicit Total Variation Diminishing (TVD) scheme recently developed for linear one-dimensional systems of hyperbolic conservation laws to the three-dimensional Navier-Stokes equations. The computation of vortical flow over a sharp-edged, thin delta wing has been chosen as a common numerical test case. The convergence of the algorithms is discussed and the accuracy of the computed flow-field results is assessed. The validity of the present results are demonstrated by a comparison with experimental data.
Document ID
19880026876
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hartwich, P. M.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Hsu, C.-H.
(Kansas, University Lawrence, United States)
Liu, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Computer Programming And Software
Meeting Information
Meeting: Applications of parallel processing in fluid mechanics
Location: Cincinnati, OH
Country: United States
Start Date: June 14, 1987
End Date: June 17, 1987
Sponsors: ASME
Accession Number
88A14103
Funding Number(s)
CONTRACT_GRANT: NAG1-455
CONTRACT_GRANT: NAS1-17919
Distribution Limits
Public
Copyright
Other

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