Active control of flow-induced cavity noise using plasma actuator

Мұқаба

Дәйексөз келтіру

Толық мәтін

Ашық рұқсат Ашық рұқсат
Рұқсат жабық Рұқсат берілді
Рұқсат жабық Тек жазылушылар үшін

Аннотация

Experimental study of high-frequency surface barrier discharge plasma actuators effect on flow-induced cavity tonal noise has been carried out. The tonal noise reduction in far field is demonstrated using two approaches: the excitation of artificial waves corresponding to high-frequency modes, and the stabilization of the flow using a plasma actuator in the feedback loop. It is shown that the stabilizing feedback loop makes it possible to significantly (by 10 dB) suppress the basic tone without the excitation of higher frequency oscillations. It is shown that this plasma actuators are able to reduce the flow cavity noise within the range of velocities (up to 60 m/s) typical for aircraft landing approach

Авторлар туралы

V. Kopiev

FAU TsAGI; FGBU OIVT RAS

Email: vkopiev@mktsagi.ru
Radio st. 17, Moscow, 105005 Russia; Izhorskaya st. 13, build. 2, Moscow, 125412 Russia

P. Kazanskii

FGBU OIVT RAS

Email: vkopiev@mktsagi.ru
Izhorskaya st. 13, build. 2, Moscow, 125412 Russia

V. Kopiev

FAU TsAGI

Email: vkopiev@mktsagi.ru
Radio st. 17, Moscow, 105005 Russia

I. Moralev

FGBU OIVT RAS

Email: vkopiev@mktsagi.ru
Izhorskaya st. 13, build. 2, Moscow, 125412 Russia

I. Pankratov

FAU TsAGI

Хат алмасуға жауапты Автор.
Email: vkopiev@mktsagi.ru
Radio st. 17, Moscow, 105005 Russia

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