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A Simplified FANG Cell-Centered Finite-Volume Method and Comparison with Other Methods for Trouble-Prone GridsWe propose a simplication of the face-averaged nodal-gradient (FANG) method for a cell-centered finite-volume Euler/Navier-Stokes solver on arbitrary grids, and compare it with other gradient methods for trouble-prone grids in two dimensions. The implementation of the FANG method is simplified by adding the face-neighbor cells of the cells around a node to a least-squares gradient stencil. The resulting method is stable for both triangular and quadrilateral grids. Although it increases the residual stencil for triangular grids, it allows the solver to work seamlessly for mixed grids and greatly simplifies the implementation, especially in three dimensions. For comparison, only explicit weighted/unweighted least-squares cell-centered and nodal gradient methods are considered. These gradients are used in both inviscid and viscous schemes, and we investigate their impact on the iterative convergence of an implicit defect-correction solver on difficult grids such as highly-curved-and-thin grids and highly distorted anisotropic grids. Finally, we will also consider a face-stencil-based limiter and compare it with a conventional cell-stencil-based limiter.
Document ID
20210015150
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hiroaki Nishikawa
(National Institute of Aerospace Hampton, Virginia, United States)
Jeffery A White
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 6, 2021
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 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)
CONTRACT_GRANT: 80LARC17C0004
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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