Studying the flowing of a wing profile in a subsonic flow in SolidWorks program
Автор: Vasina N.V.
Журнал: Теория и практика современной науки @modern-j
Рубрика: Основной раздел
Статья в выпуске: 4 (46), 2019 года.
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The paper presents a computational experiment of the process of flow past a wing profile in a subsonic flow. Considered the basic theoretical aspects and the stages of work in the program SolidWorks
Wing profile, angle of attack, aerodynamic wing quality, subsonic flow
Короткий адрес: https://sciup.org/140274491
IDR: 140274491
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