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Towards Robust and Accurate Implicit Gradient Methods for Second- and Third-Order Nodal-Gradient Cell-Centered Finite-Volume Discretizations on Tetrahedral GridsIn this paper, we introduce implicit gradient methods as alternatives to conventional least-squares gradient methods for second- and third-order nodal-gradient cell-centered finite-volume discretizations, where solutions are stored at cells but gradients are stored at nodes. Because of the unique configuration of solutions and gradients, implicit gradient systems developed for the node-centered edge-based discretization method can be directly applied once the numerical solutions are interpolated from cells to nodes with sufficient accuracy. The resulting defect-correction solver can be loosely coupled with a flow-equation solver, and at convergence, solutions and gradients that satisfy the corresponding residual equations are obtained. Each iteration is relatively cheap compared with least-squares methods involving hundreds of neighbors. Numerical results are presented for accuracy verification studies and some simple but realistic flow problems.
Document ID
20240004368
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hiroaki Nishikawa
(National Institute of Aerospace Hampton, Virginia, United States)
Date Acquired
April 11, 2024
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA Aviation 2024
Location: Las Vegas, NV
Country: US
Start Date: July 29, 2024
End Date: August 2, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80LARC23DA003
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
Computational Fluid Dynamics
Unstructured Grids
Implicit gradients
Third-order scheme
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