Implementation of the low Mach number method for calculating flows in the NOISEtte software package
- Авторы: Abalakin I.V.1, Bobkov V.G.1, Kozubskaya T.K.1
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Учреждения:
- Keldysh Institute of Applied Mathematics
- Выпуск: Том 9, № 6 (2017)
- Страницы: 688-696
- Раздел: Article
- URL: https://journals.rcsi.science/2070-0482/article/view/201979
- DOI: https://doi.org/10.1134/S2070048217060023
- ID: 201979
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Аннотация
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.
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Об авторах
I. Abalakin
Keldysh Institute of Applied Mathematics
Автор, ответственный за переписку.
Email: ilya.abalakin@gmail.com
Россия, Moscow
V. Bobkov
Keldysh Institute of Applied Mathematics
Email: ilya.abalakin@gmail.com
Россия, Moscow
T. Kozubskaya
Keldysh Institute of Applied Mathematics
Email: ilya.abalakin@gmail.com
Россия, Moscow
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