高超声速半球绕流流场电磁散射特性分析
Analysis of the scattering characteristic for the hypersonic flow field of semi-sphere
-
摘要: 分析再入流场对飞行器再入通信及空间散射特性的影响,研究电磁波与再入等离子体作用机理.采用分段线性电流密度递归卷积时域有限差分方法计算导电金属半球高超声速绕流流场电磁散射特性,分析半球等离子体包覆绕流流场雷达散射截面(RCS)随入射电磁波频率、双站角、飞行马赫数和高度变化特性.计算表明,前向是全方位散射中RCS取得最大值的方向.马赫数Ma≤10时,马赫数及高度变化对半球高超声速绕流流场L,S波段后向RCS和双站RCS影响很小;在L,S波段,绕流流场及半球本体的后向和前向RCS差距较小.马赫数Ma=14,16时,过密等离子体鞘套的形成增大了本体投影面积,在L,S波段,绕流流场前向RCS比本体前向RCS大;绕流流场存在对半球本体双站散射特性影响很大.Abstract: To understand the interaction mechanism between electromagnetic waves and reentry plasmas and the effect on the reentry communication and scattering characteristic of reentry vehicles,a piecewise linear current density recursive convolution finite-difference time-domain(PLJERC-FDTD) algorithm was applied to study the scattering characteristic for the hypersonic flow fields of conductive metal semi-sphere.The effects of incidence wave frequency,scattering angle,Mach number and altitude on the radar cross section(RCS) were analyzed.The results demonstrate that the forward RCS is the maximal RCS of all scattering orientations.The backward RCS and the bistatic RCS of flow fields vary little with Mach number and altitude for L and S wave band when the Mach number is not more than 10 in this article,and the margin of the backward RCS and the bistatic RCS between flow fields and semi-sphere is small.The forward RCS of flow fields is more than that of semi-sphere for L and S wave band because of the over-dense plasma shell when the Mach number is 14 or 16 in this article,and the difference of the bistatic scattering characteristic between flow fields and semi-sphere is obvious.
-
Key words:
- finite-difference time-domain /
- radar cross section /
- electromagnetic wave /
- plasma /
- hypersonic flow
点击查看大图
计量
- 文章访问数: 1501
- HTML浏览量: 3
- PDF量: 508
- 被引次数: 0