Edge-Based Viscous Method for Mixed-Element Node-Centered Finite-Volume Solvers

Author:

Liu Yi1,Diskin Boris,Nishikawa HiroakiORCID,Anderson William K.,Nastac Gabriel C.,Nielsen Eric J.,Walden Aaron,Wang Li

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Abstract

A novel, efficient, edge-based viscous (EBV) discretization method has been recently developed and implemented in a practical, unstructured-grid, node-centered, finite-volume flow solver. The EBV method is applied to viscous-kernel computations that include evaluations of mean-flow viscous fluxes, turbulence-model and chemistry-model diffusion terms, and the corresponding Jacobian contributions. Initially, the EBV method had been implemented for tetrahedral grids and demonstrated multifold acceleration of all viscous-kernel computations. This paper presents an extension of the EBV method for mixed-element grids. In addition to the primal edges of a given mixed-element grid, virtual edges are introduced to connect cell nodes that are not connected by a primal edge. The EBV method uses an efficient loop over all (primal and virtual) edges and features a compact discretization stencil based on the nearest neighbors. This study verifies the EBV method and assesses its efficiency on mixed-element grids by comparing the EBV solution accuracy and iterative convergence with those of well-established solutions obtained using a cell-based viscous (CBV) discretization method. The EBV solver’s memory footprint is optimized and often smaller than the memory footprint of the CBV solver. An EBV implementation of a nonlinear extension of the Spalart–Allmaras turbulence model, SA-neg-QCR2000, is also presented and verified. The SA-neg-QCR2000 model is used for simulating turbulent corner flows. Multifold speedup is demonstrated for all viscous-kernel computations, resulting in significant reduction of the time to solutions for several benchmark mixed-element-grid computations, including simulations of subsonic flows around a hemisphere–cylinder configuration and a NASA juncture-flow model, a supersonic flow through a long square duct, and a hypersonic, chemically reacting flow around a blunt body.

Funder

the U.S. Army Research Office

NASA Langley Research Center cooperative agreement with the National Institute of Aerospace

The Transformative Tools and Technologies (TTT) project of the Transformative Aeronautics Concepts Program

the NASA Revolutionary Vertical Lift Technology (RVLT) project within the NASA Aeronautics Research Mission Directorate

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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