高超声速流场等离子体逆向喷流减阻特性

doi:10.7527/S1000-6893.2022.27727

Abstract

Abstract:

Plasma Synthetic Jet （PSJ） is a high-temperature， high-speed and zero-net mass flux jet generated by arc discharge in a semi-closed cavity， with the advantages of high jet velocity， strong penetration ability and fast response， thus having significant application potential in the flow control of hypersonic vehicles. To study the flow control and drag reduction effect of the PSJ on hypersonic vehicles， we numerically simulate the bluff body model in the Mach 6 flow field. The results show that the PSJ can significantly change the shock wave distance and drag characteristics. Within a cycle after discharge， the average drag can be reduced by 37.67%， the maximum drag reduction effect can reach 76.03%， the effect of shock wave control and flow drag reduction by the PSJ is verified， and the conversion mechanism of the short penetration mode and long penetration mode of the flow field is analyzed.

Key words: hypersonic, Plasma Synthetic Jet (PSJ), opposing jet, flow control, drag reduction, mode

CLC Number:

V211

Xudong ZHANG, Zheng LI, Hao DONG, Siyuan GAO, Zubi JI, Kaixin LI, Guanghui BAI. Drag reduction characteristics of opposing plasma synthetic jet in hypersonic flow[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 115-123.

Figures/Tables 16

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Table 1

References 26

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半径/mm	最大减阻效果/%	平均减阻效果/%	控制时长/μs
1	28.75	10.80	736.6
2	62.81	16.26	474.6
3	73.92	37.58	294.5
4	76.03	37.67	253

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Drag reduction characteristics of opposing plasma synthetic jet in hypersonic flow

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