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2-D/Axisymmetric Formulation of Multi-dimensional Upwind SchemeA multi-dimensional upwind discretization of the two-dimensional/axisymmetric Navier-Stokes equations is detailed for unstructured meshes. The algorithm is an extension of the fluctuation splitting scheme of Sidilkover. Boundary conditions are implemented weakly so that all nodes are updated using the base scheme, and eigen-value limiting is incorporated to suppress expansion shocks. Test cases for Mach numbers ranging from 0.1-17 are considered, with results compared against an unstructured upwind finite volume scheme. The fluctuation splitting inviscid distribution requires fewer operations than the finite volume routine, and is seen to produce less artificial dissipation, leading to generally improved solution accuracy.
Document ID
20010066918
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wood, William A.
(NASA Langley Research Center Hampton, VA United States)
Kleb, William L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2001-2630
Report Number: AIAA Paper 2001-2630
Meeting Information
Meeting: 15th AIAA Computational Fluid Dynamics Conference
Location: Anaheim, CA
Country: United States
Start Date: June 11, 2001
End Date: June 14, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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