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二维机翼雷达散射截面特性分析
Analysis on RCS Characteristics of 2-Dimensional Airplane Wing
【摘要】 以时域有限差分法(FDTD)计算了不同后掠角的后掠翼和三角翼的雷达散射截面(RCS),并对其分布情况进行了分析;计算了不同后掠角的后掠翼和三角翼在多个频段的RCS,并按照不同的威胁判断求出平均值,得出RCS随频率的变化情况。通过分析RCS随方位和频率的变化情况,研究了外形隐身技术运用的一般原则,并探讨了吸波材料所需的最佳吸收频率和涂覆位置。通过对简化情况的分析,对雷达隐身技术运用的一般原则进行了讨论,对于实际的复杂工程实践有重要的参考价值。
【Abstract】 Different sweepback sweepback-wing and triangle-wing′s radar cross section(RCS)are computed with finite difference time domain(FDTD),and the profiles for the RCS are analyzed.Different sweepback-wing and trianglewing′s RCS in a lot of wave bands are computed,and the variety of RCS when frequency changes is obtained according to the mean value for different dangerous region.The principle of the shape-stealth technology is investigated by analyzing the RCS profiles in situation and frequency.The best-absorbing frequency and place for using absorbing material are discussed.The principia of radar stealth are discussed by predigested instance,and may do some help in complex engineering practice.
【Key words】 radar cross section(RCS); stealth; finite difference time domain(FDTD);
- 【文献出处】 飞机设计 ,Aircraft Design , 编辑部邮箱 ,2008年01期
- 【分类号】V224
- 【下载频次】179