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When the aircraft moves through the atmosphere at a very high speed, the aircraft will experience intense friction with the surrounding atmosphere, which causes the air to be ionized into plasma, thus producing a plasma flow field around it. Plasma is constantly generated on the windward side of the aircraft and flows backwards. The velocity of plasma is different from that of the aircraft. In addition to the dispersion characteristics of the plasma and the non-uniform distribution around the target, the plasma flow field will produce the effects of amplitude, frequency and phase modulation on the incident radar wave, which will change the electromagnetic scattering characteristics of the target. In order to reproduce the non-uniform Doppler phenomenon in the flow field under electromagnetic wave irradiation, the plasma echo spectrum is measured experimentally in the JF-10 wind tunnel of the Institute of Mechanics, the Chinese Academy of Sciences. The echo spectrum data of S band and C band are obtained by using a measurement system composed of signal source, circulator, antenna and spectrometer, and based on the measured data the one-dimensional range profile of the plasma coated target is simulated, and the results show that the plasma flow field has a spectrum modulation effect on the target. When the speed of the flow field cannot be compensated for accurately, the spectral modulation effect will further cause the one-dimensional range profile to defocus, which will affect the ability of radar to detect and track the object. The preliminary analysis shows that the effect is caused mainly by the inhomogeneous velocity distribution of plasma flow field and the sudden change of medium parameters when the shock wave arrives. This experiment can provide data support for verifying the electromagnetic characteristics modeling method of plasma flow field. -
Keywords:
- plasma flow field /
- spectrum modulation /
- one-dimensional range profile /
- wind tunnel
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Google Scholar
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Zeng M 2006 Ph. D. Dissertation (Beijing: Institute of Mechanics, Chinese Academy of Sciences) (in Chinese)
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图 1 试验布局示意图
Figure 1. Schematic layout of the experiment.
图 2 模型示意图
Figure 2. Schematic diagram of the model.
图 3 S波段测量结果-时频图
Figure 3. Time frequency diagram of the S-band measurement results.
图 4 C波段测量结果-时频图
Figure 4. Time frequency diagram of the C-band measurement results.
图 5 等离子体绕流场速度分解示意图
Figure 5. Schematic diagram of velocity decomposition of plasma flow field.
图 6 等离子体绕流场径向速度分布
Figure 6. Radial velocity distribution of plasma flow field.
图 7 等离子体绕流场电子密度分布
Figure 7. Electron density distribution of plasma flow field.
图 8 各散射点对应的速度和回波功率
Figure 8. Velocity and echo power corresponding to the scattering point.
图 9 一维距离像结果
Figure 9. One-dimensional range profile results.
表 1 试验段核心区气流平均参数
Table 1. Average airflow parameters in the core area of the test section.
参数 取值 ${\rho _\infty }$/(kg·m–3) 6.974 × 10–4 ${p_\infty }$/Pa 118.0 $ {T_\infty } $/K 306.8 $ {T_{v\infty }} $/K 3382 ${V_\infty }$/(m·s–1) 5173 组元
质量
分数$ C_{\rm N^2} $ 0.7456 $ C_{\rm O^2} $ 5.464 × 10–2 CN 5.324 × 10–9 CO 0.1593 CNO 4.049 × 10–2 $ C_{\rm {NO}^+} $ $ C_{\rm {NO}^+} $ 
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[1] Atatom T K 2018 IEEE Trans. Plasma Sci. 46 494
Google Scholar
[2] Khan W, Ali M, Habib Y 2020 IEEE Trans. Plasma Sci. 48 2996
Google Scholar
[3] 吴巍, 刘方, 钟建林, 王国宏 2019 电波科学学报 34 610
Google Scholar
Wu W, Liu F, Zhong J L, Wang G H 2019 Chin. J. Radio Sci. 34 610
Google Scholar
[4] 喻明浩 2019 物理学报 68 185202
Google Scholar
Yu M H 2019 Acta Phys. Sin. 68 185202
Google Scholar
[5] 韦笑, 彭世鏐, 殷红成, 印国泰 2011 系统工程与电子技术 33 506
Google Scholar
Wei X, Peng S L, Yin H C, Yin G T 2011 J. Syst. Eng. Electron. 33 506
Google Scholar
[6] Tai C T 1964 Proc. IEEE 52 685
Google Scholar
[7] Costen R C, Adamson D 1965 Proc. IEEE 53 1181
Google Scholar
[8] Yeh C, Casey K F 1966 Phys. Rev. 144 665
Google Scholar
[9] 郭琳静 2018 博士学位论文 (西安: 西安电子科技大学)
Guo L J 2018 Ph. D. Dissertation (Xi’an: Xidian University) (in Chinese)
[10] Ling H, Kim H, Hallock G A, Birkner B W 1991 IEEE Trans. Antennas Propag. 39 1412
Google Scholar
[11] 杨利霞, 谢应涛, 王祎君 2009 强激光与粒子束 21 1710
Yang L X, Xie Y T, Wang Y J 2009 High Power Laser Part. Beams 21 1710
[12] 杨利霞, 于萍萍, 马辉 2012 电波科学学报 27 18
Google Scholar
Yang L X, Yu PP, Ma H 2012 Chin. J. Radio Sci. 27 18
Google Scholar
[13] Hayami R A 1994 AIAA 17th Aerospace ground testing conference Nashville, TN, USA, July 6–8, 1992 p16
[14] Dunn M G 1970 4th Plasma Sheath Symposium Hampton Virginia, USA, October 13–15, 1970 p261
[15] 马平, 石安华, 杨益兼 2015 强激光与粒子束 27 145
Google Scholar
Ma P, Shi A H, Yang Y Q 2015 High Power Laser Part. Beams 27 145
Google Scholar
[16] 马平, 石安华, 杨益兼, 于哲峰, 梁世昌, 黄洁 2017 物理学报 66 102401
Google Scholar
Ma P, Shi A H, Yang Y Q, Yu Z F, Liang S C, Huang J 2017 Acta Phys. Sin. 66 102401
Google Scholar
[17] 马平, 石安华, 杨益兼 2017 兵工学报 38 1223
Google Scholar
Ma P, Shi A H, Yang Y Q 2017 Acta Armam. 38 1223
Google Scholar
[18] 于哲峰, 陈旭明, 杨鹰 2019 兵工学报 40 2467
Google Scholar
Yu Z F, Chen X M, Yang Y 2019 Acta Armam. 40 2467
Google Scholar
[19] 马昊军, 王国林, 罗杰, 刘丽萍, 潘德贤, 张军, 邢英丽, 唐飞 2018 物理学报 67 025201
Google Scholar
Ma H J, Wang G L, Luo J, Liu L P, Pan D X, Zhang J, Xing Y L, Tang F 2018 Acta Phys. Sin. 67 025201
Google Scholar
[20] 金铭, 韦笑, 吴洋, 张羽淮, 余西龙 2015 物理学报 64 205205
Google Scholar
Jin M, Wei X, Wu Y, Zhang Y H, Yu X L 2015 Acta Phys. Sin. 64 205205
Google Scholar
[21] 曾明 2006 博士学位论文 (北京: 中国科学院力学研究所)
Zeng M 2006 Ph. D. Dissertation (Beijing: Institute of Mechanics, Chinese Academy of Sciences) (in Chinese)
[22] Zeng M, Xu D, Liu J, Qin N. 2016 J. Thermophys. Heat Transfer 30 12
Google Scholar
[23] 宁超, 耿旭朴, 王超, 黄培康 2014 雷达学报 3 142
Google Scholar
Ning C, Geng X P, Wang C, Huang P K 2014 J. Radars 3 142
Google Scholar
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