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Cause and Cure - Deterioration in Accuracy of CFD Simulations with Use of High-Aspect-Ratio Triangular/Tetrahedral GridsTraditionally high-aspect ratio triangular/tetrahedral meshes are avoided by CFD researchers in the vicinity of a solid wall, as it is known to reduce the accuracy of gradient computations in those regions. Although for certain complex geometries, the use of high-aspect ratio triangular/tetrahedral elements in the vicinity of a solid wall can be replaced by quadrilateral/prismatic elements, ability to use triangular/tetrahedral elements in such regions without any degradation in accuracy can be beneficial from a mesh generation point of view. The benefits also carry over to numerical frameworks such as the space-time conservation element and solution element (CESE), where simplex elements are the mandatory building blocks. With the requirement of the CESE method in mind, a rigorous mathematical framework that clearly identifies the reason behind the difficulties in use of such high-aspect ratio simplex elements is formulated using two different approaches and presented here. Drawing insights from the analysis, a potential solution to avoid that pitfall is also provided as part of this work. Furthermore, through the use of numerical simulations of practical viscous problems involving high-Reynolds number flows, how the gradient evaluation procedures of the CESE framework can be effectively used to produce accurate and stable results on such high-aspect ratio simplex meshes is also showcased.
Document ID
20170007699
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Chang, Sin-Chung
(NASA Glenn Research Center Cleveland, OH United States)
Chang, Chau-Lyan
(NASA Langley Research Center Hampton, VA United States)
Venkatachari, Balaji Shankar
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
August 11, 2017
Publication Date
June 5, 2017
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN42368
Meeting Information
Meeting: AIAA Aviation 2017
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.03.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
CESE Method
mathematical
CFD
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