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A time accurate finite volume high resolution scheme for three dimensional Navier-Stokes equationsA time accurate, three-dimensional, finite volume, high resolution scheme for solving the compressible full Navier-Stokes equations is presented. The present derivation is based on the upwind split formulas, specifically with the application of Roe's (1981) flux difference splitting. A high-order accurate (up to the third order) upwind interpolation formula for the inviscid terms is derived to account for nonuniform meshes. For the viscous terms, discretizations consistent with the finite volume concept are described. A variant of second-order time accurate method is proposed that utilizes identical procedures in both the predictor and corrector steps. Avoiding the definition of midpoint gives a consistent and easy procedure, in the framework of finite volume discretization, for treating viscous transport terms in the curvilinear coordinates. For the boundary cells, a new treatment is introduced that not only avoids the use of 'ghost cells' and the associated problems, but also satisfies the tangency conditions exactly and allows easy definition of viscous transport terms at the first interface next to the boundary cells. Numerical tests of steady and unsteady high speed flows show that the present scheme gives accurate solutions.
Document ID
19890054466
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liou, Meng-Sing
(NASA Lewis Research Center Cleveland, OH, United States)
Hsu, Andrew T.
(NASA Lewis Research Center; Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-1994
Meeting Information
Meeting: AIAA Computational Fluid Dynamics Conference
Location: Buffalo, NY
Country: United States
Start Date: June 13, 1989
End Date: June 15, 1989
Accession Number
89A41837
Distribution Limits
Public
Copyright
Other

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