4.7 Article

Development of an algebraic fractional step scheme for the primitive formulation of the compressible Navier-Stokes equations

期刊

JOURNAL OF COMPUTATIONAL PHYSICS
卷 433, 期 -, 页码 -

出版社

ACADEMIC PRESS INC ELSEVIER SCIENCE
DOI: 10.1016/j.jcp.2020.110017

关键词

Compressible flow; Variational multiscale method; Fractional step schemes; Finite element method; Weak imposition of boundary conditions

资金

  1. Agencia de Gestio d'Ajuts Universitaris i de Recerca [2019-FI-B-00607]
  2. Spanish Government [RYC-2015-17367, TOP-FSI: RTI2018-098276-B-I00]
  3. ICREA Academia Research Program of the Catalan Government
  4. Spanish Ministry of Economy and Competitiveness [CEX2018-000797-S]

向作者/读者索取更多资源

This work presents a finite-element solver based on a fractional step scheme for the compressible Navier-Stokes equations in the primitive formulation, which allows for cost savings and decoupling of unknowns calculation. The methodology includes improvements in stabilization techniques and a method for addressing wave reflections. Several benchmark simulations demonstrate the algorithm's suitability for subsonic flows.
In this work we address the compressible Navier-Stokes equations written in the so-called primitive formulation. The proposed methodology is a finite-element solver based on a fractional step scheme in time, which allows to uncouple the calculation of the problem unknowns providing important savings in computational cost. In addition, we include a stabilization technique within the Variational Multi-Scale framework and, in particular, we consider orthogonal and dynamic definitions for the subscales. In order to overcome any wave reflections which may arise in aeroacoustic simulations at the low compressibility regime, we present a method for enforcing boundary conditions based on a combination of a zero order non-reflecting condition plus the weak imposition of Dirichlet boundary conditions over the external contours. Several representative benchmark flow simulations are performed, which demonstrate the suitability of the proposed algorithm for the subsonic regime. (C) 2020 Elsevier Inc. All rights reserved.

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