Thrust-Energy Characteristics of Plasma Actuators at Various Pressures


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Resumo

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.

Sobre autores

V. Bocharnikov

Joint Institute for High Temperatures, Russian Academy of Sciences

Autor responsável pela correspondência
Email: vova.m.bocha@gmail.com
Rússia, 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
Rússia, Moscow, 127412; Dolgoprudnyi, Moscow oblast, 141700

V. Golub

Joint Institute for High Temperatures, Russian Academy of Sciences

Email: vova.m.bocha@gmail.com
Rússia, Moscow, 127412


Declaração de direitos autorais © Pleiades Publishing, Ltd., 2018

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