Аннотация
We propose a numerical method for a supersonic van der Waals gas flow about a round cone. This method enables one to calculate shock waves attached to the cone and flow parameters between the shock wave and the surface area of the cone. The advantages of the algorithm are demonstrated on some examples.
Язык оригинала | английский |
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Номер статьи | 012009 |
Число страниц | 7 |
Журнал | Journal of Physics: Conference Series |
Том | 894 |
Номер выпуска | 1 |
DOI | |
Состояние | Опубликовано - 22 окт. 2017 |