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Adaptive mesh generation for viscous flows using Delaunay triangulationA method for generating an unstructured triangular mesh in two dimensions, suitable for computing high Reynolds number flows over arbitrary configurations is presented. The method is based on a Delaunay triangulation, which is performed in a locally stretched space, in order to obtain very high aspect ratio triangles in the boundary layer and the wake regions. It is shown how the method can be coupled with an unstructured Navier-Stokes solver to produce a solution adaptive mesh generation procedure for viscous flows.
Document ID
19880020365
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mavriplis, Dimitri J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-181699
NAS 1.26:181699
ICASE-88-47
Report Number: NASA-CR-181699
Report Number: NAS 1.26:181699
Report Number: ICASE-88-47
Accession Number
88N29749
Funding Number(s)
CONTRACT_GRANT: NAS1-18107
PROJECT: RTOP 505-90-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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