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Assessment of Edge-Based Viscous Method for Corner-Flow Solutions on Graphics Processing UnitsA highly efficient, edge-based viscous (EBV) discretization method has been recently implemented in a practical, unstructured-grid, node-centered, finite-volume flow solver and evaluated for Reynolds-averaged Navier-Stokes (RANS) formulations. In comparison to a well-established cell-based viscous (CBV) method, the EBV method has demonstrated multifold acceleration of all viscous-kernel computations on general unstructured mixed-element grids. The viscous kernels include evaluation of viscous fluxes, diffusion terms in turbulence models, and the corresponding Jacobian terms. In this paper, an EBV implementation of a nonlinear extension of the Spalart-Allmaras turbulence model, SA-neg-QCR2000, is presented and verified. The SA-neg-QCR2000 model is used for simulating turbulent corner flows. Previously reported EBV computations have been conducted on traditional computing architectures based on central processing units (CPU). This paper assesses benefits of the EBV method on modern high-performance computing architectures based on graphics processing units (GPU). The GPU implementations of the CBV and EBV methods are verified by comparing solutions and iterative convergence with those observed in CPU computations on the same grids. A comprehensive assessment of the EBV speedup on CPU and GPU architectures is presented for established benchmark corner flows, namely, a supersonic flow through a long square duct and a subsonic flow around a NASA juncture flow model.
Document ID
20220016998
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Yi Liu
(National Institute of Aerospace Hampton, Virginia, United States)
Boris Diskin
(National Institute of Aerospace Hampton, Virginia, United States)
Hiroaki Nishikawa
(National Institute of Aerospace Hampton, Virginia, United States)
William K. Anderson
(Langley Research Center Hampton, Virginia, United States)
Gabriel C. Nastac
(Langley Research Center Hampton, Virginia, United States)
Eric J. Nielsen
(Langley Research Center Hampton, Virginia, United States)
Aaron Walden
(Langley Research Center Hampton, Virginia, United States)
Li Wang
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 9, 2022
Subject Category
Aerodynamics
Numerical Analysis
Meeting Information
Meeting: AIAA SciTech Forum
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0004
CONTRACT_GRANT: NNL09AA00A
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
CFD
Edge-based Viscous Method
finite-volume discretization
GPU
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