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Multigrid solution of the Navier-Stokes equations on triangular meshesA Navier-Stokes algorithm for use on unstructured triangular meshes is presented. Spatial discretization of the governing equations is achieved using a finite element Galerkin approximation, which can be shown to be equivalent to a finite volume approximation for regular equilateral triangular meshes. Integration steady-state is performed using a multistage time-stepping scheme, and convergence is accelerated by means of implicit residual smoothing and an unstructured multigrid algorithm. Directional scaling of the artificial dissipation and the implicit residual smoothing operator is achieved for unstructured meshes by considering local mesh stretching vectors at each point. The accuracy of the scheme for highly stretched triangular meshes is validated by comparing computed flat-plate laminar boundary layer results with the well known similarity solution, and by comparing laminar airfoil results with those obtained from various well-established structured quadrilateral-mesh codes. The convergence efficiency of the present method is also shown to be competitive with those demonstrated by structured quadrilateral-mesh algorithms.
Document ID
19900060256
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mavriplis, D. J.
(NASA Langley Research Center Hampton, VA, United States)
Jameson, A.
(Princeton University NJ, United States)
Date Acquired
August 14, 2013
Publication Date
August 1, 1990
Publication Information
Publication: AIAA Journal
Volume: 28
ISSN: 0001-1452
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0001-1452
Accession Number
90A47311
Distribution Limits
Public
Copyright
Other

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