Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций
Конференция: Siberian Thermophysical Seminar, STS 2021
Год издания: 2021
Идентификатор DOI: 10.1088/1742-6596/2119/1/012154
Аннотация: An experimental and computational study of the NACA0016 airfoil has been carried out for two cases: a stationary airfoil in an incoming flow on an aerodynamic stand and an airfoil moving along a circular trajectory in a stationary flow in a hydrodynamic stand. The Reynolds number for both cases was 60000. A qualitative comparison of the velocity fields for the cases with smooth airflow and boundary layer separation was carried out. It is shown that the used calculation methods describe the task under study with sufficient quality. © 2021 Institute of Physics Publishing. All rights reserved.
Издание
Журнал: Journal of Physics: Conference Series
Выпуск журнала: Vol. 2119, Is. 1
Номера страниц: 12154
ISSN журнала: 17426588
Издатель: IOP Publishing Ltd
Персоны
- Bozheeva D.M. (Siberian Federal University, 79 Svobodny pr., Krasnoyarsk, 660041, Russian Federation)
- Dekterev D.A. (Institute of Thermophysics SB RAS, 1 Acad. Lavrentiev pr., Novosibirsk, 630090, Russian Federation, Siberian Federal University, 79 Svobodny pr., Krasnoyarsk, 660041, Russian Federation)
- Dekterev Ar.A. (Institute of Thermophysics SB RAS, 1 Acad. Lavrentiev pr., Novosibirsk, 630090, Russian Federation)
- Dekterev A.A. (Institute of Thermophysics SB RAS, 1 Acad. Lavrentiev pr., Novosibirsk, 630090, Russian Federation, Siberian Federal University, 79 Svobodny pr., Krasnoyarsk, 660041, Russian Federation)
- Platonov D.V. (Institute of Thermophysics SB RAS, 1 Acad. Lavrentiev pr., Novosibirsk, 630090, Russian Federation, Siberian Federal University, 79 Svobodny pr., Krasnoyarsk, 660041, Russian Federation)
Вхождение в базы данных
Информация о публикациях загружается с сайта службы поддержки публикационной активности СФУ. Сообщите, если заметили неточности.