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Edge Based Viscous Method for Node-Centered FormulationsThis paper presents a novel, efficient, conservative, edge-based method for evaluation of mean flow viscous fluxes and turbulence-model diffusion terms of the Reynolds-averaged Navier-Stokes equations on tetrahedral grids. The new method is implemented in a practical, node-centered, finite-volume computational fluid dynamics solver. The baseline finite-volume scheme that is equivalent to a second-order accurate finite-element Galerkin approximation of viscous stresses is reformulated. The order of operations to compute the cell-based Green-Gauss gradients is changed to combine the operations by edge, which leads to an equivalent formulation on tetrahedral grids, improves efficiency, and preserves the compact discretization stencil based on the nearest neighbors. The computational results presented in this paper verify the implementation of this edge-based method by comparing its accuracy and iterative convergence with those of the well verified and validated baseline formulation. Efficiency gains for residual and Jacobian evaluations result in significant reduction of time to solution. This novel edge-based formulation on tetrahedra can be seamlessly combined with the baseline formulation on cells of other types for computing solutions on mixed-element grids.
Document ID
20210016186
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Yi Liu
(National Institute of Aerospace Hampton, Virginia, United States)
Boris Diskin
(National Institute of Aerospace Hampton, Virginia, United States)
William K Anderson
(Langley Research Center Hampton, Virginia, United States)
Eric J Nielsen
(Langley Research Center Hampton, Virginia, United States)
Li Wang
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 24, 2021
Subject Category
Air Transportation And Safety
Meeting Information
Meeting: 2021 AIAA Aviation Forum
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109494.02.07.05.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Edge Based
FUN3D
CFD
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