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典型文献
Experimental study on surface arc plasma actuation-based hypersonic boundary layer transition flow control
文献摘要:
Effective control of hypersonic transition is essential.In order to avoid affecting the structural profile 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 the Ф0.25 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.
文献关键词:
作者姓名:
Hesen YANG;Hua LIANG;Shanguang GUO;Yanhao LUO;Mengxiao TANG;Chuanbiao ZHANG;Yun WU;Yinghong LI
作者机构:
Science and Technology on Plasma Dynamics Laboratory,Air Force Engineering University,Xi'an 710038,People's Republic of China;School of Mechanical Engineering,Xi'an Jiaotong University,Xi'an 710048,People's Republic of China
引用格式:
[1]Hesen YANG;Hua LIANG;Shanguang GUO;Yanhao LUO;Mengxiao TANG;Chuanbiao ZHANG;Yun WU;Yinghong LI-.Experimental study on surface arc plasma actuation-based hypersonic boundary layer transition flow control)[J].等离子体科学和技术(英文版),2022(09):108-116
A类:
Contacting
B类:
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AB值:
0.597432
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