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Experimental study on surface arc plasma actuation-based hypersonic boundary layer transition flow control 被引量:2
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作者 Hesen YANG Hua LIANG +5 位作者 Shanguang GUO Yanhao LUO Mengxiao TANG Chuanbiao ZHANG Yun WU Yinghong LI 《Plasma Science and Technology》 SCIE EI CAS CSCD 2022年第9期108-116,共9页
Effective control of hypersonic transition is essential.In order to avoid affecting the structural proflle of the aircraft,as well as reducing power consumption and electromagnetic interference,a low-frequency surface... Effective control of hypersonic transition is essential.In order to avoid affecting the structural proflle of the aircraft,as well as reducing power consumption and electromagnetic interference,a low-frequency surface arc plasma disturbance experiment to promote hypersonic transition was carried out in theΦ0.25 m double-throat Ludwieg tube wind tunnel at Huazhong University of Science and Technology.Contacting printed circuit board sensors and non-contact focused laser differential interferometry testing technology were used in combination.Experimental results showed that the low-frequency surface arc plasma actuation had obvious stimulation effects on the second-mode unstable wave and could promote boundary layer transition by changing the spectral characteristics of the second-mode unstable wave.At the same time,the plasma actuation could promote energy exchange between the second-mode unstable wave and other unstable waves.Finally,the corresponding control mechanism is discussed. 展开更多
关键词 plasma actuation flow control surface arc discharge hypersonic boundary layer transition experimental study
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