摘要
从直升机旋翼的散射积分方程出发，用矩量法对直升机旋翼在垂直入射和掠入射两种。情形下的静态后向散射截面（ＲＣＳ）进行了理论预估。
In this paper the EFIE for the helicopter rotor is built, and the maximum values of the theoretic RCS for helicopter rotor are predicated by using of MOM, in case of the vertical incidence and the closing to horizon incidence, respectively.
出处
《空军雷达学院学报》
2001年第2期4-6,共3页
Journal of Air Force Radar Academy
关键词
直升机旋翼
矩量法
RCS
helicopter rotor
method of moment (MOM)
RCS
