Отправить статью по E-mail Thrust-Energy Characteristics of Plasma Actuators at Various Pressures
- Авторы: Bocharnikov V.1, Trifanov I.1,2, Golub V.1
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Учреждения:
- Joint Institute for High Temperatures, Russian Academy of Sciences
- Moscow Institute of Physics and Technology (State University)
- Выпуск: Том 45, № 1 (2019)
- Страницы: 31-33
- Раздел: Article
- URL: https://journals.rcsi.science/1063-7850/article/view/208185
- DOI: https://doi.org/10.1134/S1063785019010206
- ID: 208185
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Аннотация
We have studied the pressure dependences of the long thrust and specific power thrust of synthetic jets generated by dielectric barrier discharge of a symmetric actuator at reduced pressures. Decreasing pressure leads to increase in the length of the plasma sheet. The thrust of synthetic jets reaches a maximum at a certain pressure dependent on the actuator geometry.
Об авторах
V. Bocharnikov
Joint Institute for High Temperatures, Russian Academy of Sciences
Автор, ответственный за переписку.
Email: vova.m.bocha@gmail.com
Россия, Moscow, 127412
I. Trifanov
Joint Institute for High Temperatures, Russian Academy of Sciences; Moscow Institute of Physics and Technology (State University)
Email: vova.m.bocha@gmail.com
Россия, Moscow, 127412; Dolgoprudnyi, Moscow oblast, 141700
V. Golub
Joint Institute for High Temperatures, Russian Academy of Sciences
Email: vova.m.bocha@gmail.com
Россия, Moscow, 127412
