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Updates to Implicit Edge-Based Gradient MethodsIn this paper, we report updates to the implicit edge-based gradient methods originally introduced in [H. Nishikawa, AIAA Paper 2020-3048, 2020]. First, we clarify the relationship between gradient accuracy and truncation error and show that the quadratic method involves a free parameter. Then, we provide a complete description and a simplified matrix form of the implicit gradient systems including a consistent boundary treatment, and derive a set of parameters for achieving fourth-order gradient accuracy on regular tetrahedral grids. A stability analysis is performed for a relaxation scheme used to solve the implicit gradient systems, and the result serves as a guide for choosing parameters. Numerical results are shown for accuracy verification and also for realistic inviscid flow problems in three dimensions, including flows with shock waves.
Document ID
20230015557
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hiroaki Nishikawa
(National Institute of Aerospace Hampton, Virginia, United States)
Date Acquired
October 27, 2023
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80LARC23DA003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Weighted Least-Squares
Computational Fluid Dynamics
Hypersonic Flow
Gradient Limiters
Unstructured Grids
Adapted Grids
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