高超声速流场等离子体合成射流逆向喷流特性

doi:10.7527/S1000-6893.2022.27747

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高超声速流场等离子体合成射流逆向喷流特性

马正雪¹, 罗振兵¹(), 赵爱红², 周岩¹, 谢玮¹, 刘强¹, 朱寅鑫¹, 彭文强¹

^1.国防科技大学空天科学学院，长沙 410073
^2.中国运载火箭技术研究院空间物理重点实验室，北京 100076

收稿日期:2022-07-01 修回日期:2022-07-29 接受日期:2022-08-25 出版日期:2022-12-25 发布日期:2022-09-13
通讯作者: 罗振兵 E-mail:luozhenbing@163.com
基金资助:
国家自然科学基金(12002377);国家科技重大专项（J2019-Ⅲ-0010-0054）

Reverse jet characteristics of plasma synthetic jet in hypersonic flow field

Zhengxue MA¹, Zhenbing LUO¹(), Aihong ZHAO², Yan ZHOU¹, Wei XIE¹, Qiang LIU¹, Yinxin ZHU¹, Wenqiang PENG¹

^1.College of Aerospace Science and Engineering，National University of Defense Technology，Changsha 410073，China
^2.Science and Technology on Space Physics Laboratory，China Academy of Launch Vehicle Technology，Beijing 100076，China

Received:2022-07-01 Revised:2022-07-29 Accepted:2022-08-25 Online:2022-12-25 Published:2022-09-13
Contact: Zhenbing LUO E-mail:luozhenbing@163.com
Supported by:
National Natural Science Foundation of China(12002377);National Science and Technology Major Project（J2019-Ⅲ-0010-0054）

摘要/Abstract

摘要：

为了研究在高超声速条件下逆向等离子体合成射流流场特性，进行了试验和数值研究。在马赫数为8的高超声速来流中，通过比较试验和仿真中纹影以及激励器出口压力监测结果，分析了反向等离子体合成射流的流场变化。验证了高超声速条件下，反向等离子体合成射流激励器出口压力振荡，是腔体内多次回填产生多次喷流导致多道激波扫过激励器出口所导致的；等离子体合成射流增大了射流区域外的气体质量流量，同时向上游传播的前驱激波与弓形激波融合为一道激波；在高动量射流的作用下产生的涡环、逆流产生的低压区以及高温低密度等离子体射流降低了当地马赫数，使得激波穿透深度增加。

关键词: 等离子体合成射流, 流动控制, 高超声速来流, 逆向喷流, 穿透深度

Abstract:

To study the flow field characteristics of the reverse plasma synthetic jet under hypersonic conditions， experimental and numerical studies were carried out. In the hypersonic incoming flow with Mach number 8， the flow field variation of the reverse plasma synthetic jet was analyzed by comparing the schlieren and exciter outlet pressure monitoring results in the experiment and simulation. It is verified that under hypersonic conditions， the outlet pressure oscillation of the reverse plasma synthesis jet actuator is caused by multiple jets generated by multiple backfilling in the cavity， causing multiple shocks to sweep over the actuator outlet. The plasma synthesis jet increases the mass flow of the gas outside the jet area， while the precursor shock propagating upstream merges with the bow shock wave into a single shock. The vortex rings produced under the action of high-momentum jets， the low-pressure regions created by counter-currents， and the high-temperature low-density plasma jets reduce the local Mach number， resulting in an increase in the shock penetration depth.

Key words: plasma synthetic jet, flow control, hypersonic incoming flow, reverse jet, penetration depth

中图分类号:

V211.3

马正雪, 罗振兵, 赵爱红, 周岩, 谢玮, 刘强, 朱寅鑫, 彭文强. 高超声速流场等离子体合成射流逆向喷流特性[J]. 航空学报, 2022, 43(S2): 192-203.

Zhengxue MA, Zhenbing LUO, Aihong ZHAO, Yan ZHOU, Wei XIE, Qiang LIU, Yinxin ZHU, Wenqiang PENG. Reverse jet characteristics of plasma synthetic jet in hypersonic flow field[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 192-203.

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

参数	数值
喷管出口直径/m	0.5
风洞马赫数	5， 6， 7， 8
流量/（kg∙s^-1）	0.29~15.50
总压/MPa	0.04~1.0
总温/K	288~685
单位雷诺数/m^-1	6.47×10⁵~2.24×10⁷
模拟飞行高度/km	27~59
风洞运行时间/s	10
模型最大底部直径/mm	120
气源容积/m³	32
真空容积/m³	650

工况	总压 /atm	激励器腔体压力/Pa	总温 /℃	放电能量/J	电容 /μF
1	7.5	558.75	228	0.69	0.64
2	7.4	551.3	236	1.44	0.96
3	7.4	551.3	238	1.29	0.96
4	7.4	551.3	246	4.42	2.28

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高超声速流场等离子体合成射流逆向喷流特性

Reverse jet characteristics of plasma synthetic jet in hypersonic flow field

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