Experiment on Shock Wave Control of a Hypersonic Vehicle Standard Model Based on Plasma Synthetic Jet

XIE Wei; HU Guo-tun; SHI Wei; ZHOU Yan; LU Hong-bo; LUO Zhen-bing

doi:10.19527/j.cnki.2096-1642.1065

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XIE Wei, HU Guo-tun, SHI Wei, ZHOU Yan, LU Hong-bo, LUO Zhen-bing. Experiment on Shock Wave Control of a Hypersonic Vehicle Standard Model Based on Plasma Synthetic Jet[J]. PHYSICS OF GASES. doi: 10.19527/j.cnki.2096-1642.1065

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XIE Wei, HU Guo-tun, SHI Wei, ZHOU Yan, LU Hong-bo, LUO Zhen-bing. Experiment on Shock Wave Control of a Hypersonic Vehicle Standard Model Based on Plasma Synthetic Jet[J]. PHYSICS OF GASES. doi: 10.19527/j.cnki.2096-1642.1065

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Experiment on Shock Wave Control of a Hypersonic Vehicle Standard Model Based on Plasma Synthetic Jet

doi: 10.19527/j.cnki.2096-1642.1065

1. College of Aeronautics and Astronautics, National University of Defense Technology, Changsha 410073, China;
2. China Academy of Launch Vehicle Technology, Beijing 100076, China;
3. China Academy of Aerospace Aerodynamics, Beijing 100074, China

Received Date: 08 Jun 2023
Revised Date: 18 Jun 2023

Available Online: 21 Aug 2023

Abstract

Abstract

The novel active flow control technology based on plasma synthetic jet (PSJ) has great application potential in the field of shock wave control due to its advantages such as no gas source, strong control ability and wide excitation frequency band. The control effect of single-pulsed PSJ on head bow shock and wing shock of a hypersonic vehicle model and the drag reduction effect were experimentally studied in a hypersonic wind tunnel. The results show that the opposing PSJ can significantly increase the standoff distance of the head bow shock, and the transverse PSJ can basically eliminate the wing shock completely. The maximum instantaneous drag reduction rate of the vehicle measured by the dynamic force sensor is about 15.5%, but the drag change measured by the sensor has a delay of about 250 μs. The influence of discharge energy, incoming flow total pressure, exit diameter and cavity volume on the control effect of the head bow shock was also studied.
- plasma synthetic jet,
- shock wave control,
- hypersonic vehicle,
- active flow control

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References(32)

References

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Experiment on Shock Wave Control of a Hypersonic Vehicle Standard Model Based on Plasma Synthetic Jet

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Experiment on Shock Wave Control of a Hypersonic Vehicle Standard Model Based on Plasma Synthetic Jet

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