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Recent Development in the CESE Method for the Solution of the Navier-Stokes Equations Using Unstructured Triangular or Tetrahedral Meshes With High Aspect RatioIn the multidimensional CESE development, triangles and tetrahedra turn out to be the most natural building blocks for 2D and 3D spatial meshes. As such the CESE method is compatible with the simplest unstructured meshes and thus can be easily applied to solve problems with complex geometries. However, because the method uses space-time staggered stencils, solution decoupling may become a real nuisance in applications involving unstructured meshes. In this paper we will describe a simple and general remedy which, according to numerical experiments, has removed any possibility of solution decoupling. Moreover, in a real-world viscous flow simulation near a solid wall, one often encounters a case where a boundary with high curvature or sharp corner is surrounded by triangular/tetrahedral meshes of extremely high aspect ratio (up to 106). For such an extreme case, the spatial projection of a space-time compounded conservation element constructed using the original CESE design may become highly concave and thus its centroid (referred to as a spatial solution point) may lie far outside of the spatial projection. It could even be embedded beyond a solid wall boundary and causes serious numerical difficulties. In this paper we will also present a new procedure for constructing conservation elements and solution elements which effectively overcomes the difficulties associated with the original design. Another difficulty issue which was addressed more recently is the wellknown fact that accuracy of gradient computations involving triangular/tetrahedral grids deteriorates rapidly as the aspect ratio of grid cells increases. The root cause of this difficulty was clearly identified and several remedies to overcome it were found through a rigorous mathematical analysis. However, because of the length of the current paper and the complexity of mathematics involved, this new work will be presented in another paper.
Document ID
20140002883
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Chang, Sin-Chung
(NASA Glenn Research Center Cleveland, OH, United States)
Chang, Chau-Lyan
(NASA Langley Research Center Hampton, VA, United States)
Yen, Joseph C.
(Jacobs Technology Inc. Tullahoma, TN, United States)
Date Acquired
April 11, 2014
Publication Date
September 1, 2013
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper-2013-3068
NASA/TM-2013-218061
E-18704
Meeting Information
Meeting: Computational Fluid Dynamics Conference
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 599489.02.07.03.04.13.01
WBS: WBS 794072.02.03.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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