Аннотация
This paper discusses the numerical simulation of the 69-Degree Delta Wing Body for computing the sonic boom signature in the near field. For flow field calculation, the commercial CFD flow solver ANSYS Fluent is employed. The computational mesh in the perturbed flow regions was refined two times using the automatic gradient adaptation. The results are in agreement with the results obtained by other researchers.
Язык оригинала | английский |
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Номер статьи | 012112 |
Журнал | Journal of Physics: Conference Series |
Том | 1404 |
Номер выпуска | 1 |
DOI | |
Состояние | Опубликовано - 6 дек 2019 |
Событие | 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 - Novosibirsk, Российская Федерация Продолжительность: 30 сен 2019 → 5 окт 2019 |