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A mixed volume grid approach for the Euler and Navier-Stokes equationsAn approach for solving the compressible Euler and Navier-Stokes equations upon meshes composed of nearly arbitrary polyhedra is described. Each polyhedron is constructed from an arbitrary number of triangular and quadrilateral face elements, allowing the unified treatment of tetrahedral, prismatic, pyramidal, and hexahedral cells, as well the general cut cells produced by Cartesian mesh approaches. The basics behind the numerical approach and the resulting data structures are described. The accuracy of the mixed volume grid approach is assessed by performing a grid refinement study upon a series of hexahedral, tetrahedral, prismatic, and Cartesian meshes for an analytic inviscid problem. A series of laminar validation cases are made, comparing the results upon differing grid topologies to each other, to theory, and experimental data. A computation upon a prismatic/tetrahedral mesh is made simulating the laminar flow over a wall/cylinder combination.
Document ID
19960012165
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coirier, William J.
(NASA Lewis Research Center Cleveland, OH, United States)
Jorgenson, Philip C. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 96-0762
NASA-TM-107135
NIPS-96-07909
E-10065
NAS 1.15:107135
Report Number: AIAA PAPER 96-0762
Report Number: NASA-TM-107135
Report Number: NIPS-96-07909
Report Number: E-10065
Report Number: NAS 1.15:107135
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 15, 1996
End Date: January 18, 1996
Sponsors: AIAA
Accession Number
96N18402
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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