Computational grid adaptation for the sonic boom near field modeling

T. Kiseleva; V. Temerbekov

doi:10.1088/1742-6596/1404/1/012112

Computational grid adaptation for the sonic boom near field modeling

T. Kiseleva, V. Temerbekov

Кафедра общей физики ФФ

Результат исследования: Научные публикации в периодических изданиях › статья по материалам конференции › рецензирование

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
Номер статьи	012112
Журнал	Journal of Physics: Conference Series
Том	1404
Номер выпуска	1
DOI	https://doi.org/10.1088/1742-6596/1404/1/012112
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

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10.1088/1742-6596/1404/1/012112

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title = "Computational grid adaptation for the sonic boom near field modeling",

abstract = "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.",

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Computational grid adaptation for the sonic boom near field modeling. / Kiseleva, T.; Temerbekov, V.

В: Journal of Physics: Conference Series, Том 1404, № 1, 012112, 06.12.2019.

Результат исследования: Научные публикации в периодических изданиях › статья по материалам конференции › рецензирование

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AU - Temerbekov, V.

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AB - 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.

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Computational grid adaptation for the sonic boom near field modeling

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