General theory of stratified media. Applied to the research of the correction of aircraft radome errors

Ch Favier de Coulomb
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Abstract

The problem treated in this paper is the radiation disturbances of a tracking radar antenna placed in the nose of a supersonic aircraft or engin which are due to the insertion of the radome between the antenna and its environment. The two essential reasons for the errors caused by the radome are: the taperd slim form given to the radome for to keep up with aerodynamic requirements. the rotating movement of the antenna about a point centered in the radiating surface. From these two particular points it is understood that the waves starting from the antenna may cross the radome wall with important and even grazing incidence angles. Amongst the radome errors deriving from this fact and being the most undesirable one is the axis deviation of a tracking radar which we call in the following the ? radome aberration ?. The different procedures employed up to now in order to correct this aberration (local thickness variations for an example) were not completely satisfying. Hence we had to look for and to try new methods in application of new ideas. So it seems a priori to be possible to dispose of a greater number of parameters for the correction of the radome aberration by increasing the number of dielectric layers used to built up a radome wall. But the theory of satisfied media, not being simple at its base, gets rapidly still more complicated by increasing the number of dielectric layers. In the first part of the paper a general theory of electromagnetic wave propagation in stratified media, divided into an arbitrary number of dielectric layers, is established. This theory is than appplied in the second part to the study of transmission and phase of a plane wave incident on a multilayer wall at grazing angles. The research has been directed to obtain good transmission and quasi zero phase variation versus incidence, the former in order to optimize energy transmission through the radome wall, the latter in order to facilitate the correction of radome aberration thanks to small phase variation and small phase variations cause poor transmission. It is finally shown that the best compromise for the design of a engin nose radome is the monolithic wall being adapted at the limit of grazing incidence and having a high dielectric constant.
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分层介质的一般理论。应用于飞机天线罩误差的校正研究
本文研究的是放置在超音速飞机或发动机机头的跟踪雷达天线由于天线罩的插入而产生的辐射干扰问题。造成天线罩误差的两个重要原因是:为了满足气动要求,天线罩采用了锥形的细长外形。天线围绕辐射表面中心一点的旋转运动。从这两个特殊的点可以理解,从天线出发的波可能以重要的均匀掠入射角穿过天线罩壁。在由这个事实产生的天线罩误差中,最不受欢迎的是跟踪雷达的轴偏差,我们在下面称之为?天线罩畸变?。到目前为止,为了纠正这种像差(例如局部厚度变化)而采用的不同程序并不完全令人满意。因此,我们必须寻找和尝试应用新思想的新方法。因此,通过增加用于建立天线罩壁的介电层的数量,似乎可以先验地处理更多的参数来校正天线罩像差。但是,满足介质理论的基础并不简单,随着介电层数的增加,它迅速变得更加复杂。本文第一部分建立了电磁波在分层介质中传播的一般理论,这种介质被划分为任意数目的介电层。第二部分将该理论应用于入射多层壁面的平面波在掠掠角下的传输和相位的研究。研究的方向是获得良好的传输和准零相位随入射变化,前者是为了优化能量通过天线罩壁的传输,后者是为了校正天线罩像差,因为相位变化小,而相位变化小导致传输差。最后表明,对于发动机机头天线罩的设计来说,最好的折衷方案是在掠射入射的极限处采用单片壁,并具有较高的介电常数。
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