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Physical foundations of gas dynamic method of controlling subsonic gas fetes
- Authors: 1 11, 1 11, 1 11, 1 11
-
Affiliations:
- Federal State Unitary Enterprise “Moscow Machine Building Manufacturing Company” “Salyut”, Moscow
- Issue: Vol 5, No 1 (2006)
- Pages: 167-175
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/265
- DOI: https://doi.org/10.18287/2541-7533-2006-0-1%20(9)-167-175
- ID: 265
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Abstract
Making new engineering devices requires a stage of theoretical grounding of the regularity of the claimed indicators being manifested. This stage is particularly important for aircraft engine devices and units as their reliability provides the safety of operating an air vehicle as a whole. The paper offers mathematical and physical grounding of a gas dynamic method of controlling subsonic gas jets based on the use of Coanda effect.
About the authors
1 1
Federal State Unitary Enterprise “Moscow Machine Building Manufacturing Company” “Salyut”, Moscow
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
Federal State Unitary Enterprise “Moscow Machine Building Manufacturing Company” “Salyut”, Moscow
Email: sadohina@ssau.ru
Russian Federation
1 1
Federal State Unitary Enterprise “Moscow Machine Building Manufacturing Company” “Salyut”, Moscow
Email: sadohina@ssau.ru
Russian Federation
1 1
Federal State Unitary Enterprise “Moscow Machine Building Manufacturing Company” “Salyut”, Moscow
Email: sadohina@ssau.ru
Russian Federation
References
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- Флетчер К. Вычислительные методы в динамике жидкостей: В 2-х т.: Пер. с англ. - М.: Мир, 1991.
- Курант Р. Уравнения с частными производными. - М.: Мир, 1964.
- Маслов Л. А. Расчет обтекания кольцевого крыла // Ученые записки ЦАГИ. Том Х, №1. - 1979. - С. 1-9.
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