Implementation of the low Mach number method for calculating flows in the NOISEtte software package

I. V. Abalakin; V. G. Bobkov; T. K. Kozubskaya

doi:10.1134/S2070048217060023

Implementation of the low Mach number method for calculating flows in the NOISEtte software package

作者: Abalakin I.V.¹, Bobkov V.G.¹, Kozubskaya T.K.¹
隶属关系:
1. Keldysh Institute of Applied Mathematics
期: 卷 9, 编号 6 (2017)
页面: 688-696
栏目: Article
URL: https://journals.rcsi.science/2070-0482/article/view/201979
DOI: https://doi.org/10.1134/S2070048217060023
ID: 201979

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详细

This paper is devoted to the development of computational techniques for simulating low Mach number flows on unstructured meshes based on the Roe method and the edge-based vertexcentered higher accuracy schemes. The techniques are implemented in the in-house NOISEtte code. The results of predicting an inviscid compressible low Mach number flow over a NACA0012 airfoil are presented and analyzed. The computations are carried out on structured and unstructured triangular grids.