摘要
应用二维时域有限差分(FDTD)程序计算二维翼型NACA0012和金属方柱的双站雷达散射截面,与国内外文献上的结果进行比较,证明该程序的有效性.而后计算二维不同形状机翼的双站雷达散射截面(RCS)和不同后掠角时后掠翼和三角翼的双站RCS,得出不同形状机翼有不同的RCS分布;改变后掠角的大小可以改变机翼的RCS分布.因此,根据设计要求,可以通过选用不同机翼形状或不同大小的后掠角,使飞行器达到RCS减缩.
Bistatic radar cross sections (RCS) of NACA0012 and a square-pole of metal are computed with 2D FDTD program. Numerical results are consistent with those of literature available. Hence the 2D FDTD program is shown correct and effective. Calculations are performed for the bistatic RCS of 2D wings, sweepback-wings and triangle-wings. These results show that wings with different figure have different profiles of RCS and varying angle χ causes the change of sweepback-wing and triangle-wing's RCS. The requirement of reducing RCS could be reached through choosing different figure of wing or varying χ according to the design demand.
出处
《计算物理》
EI
CSCD
北大核心
2005年第1期65-69,共5页
Chinese Journal of Computational Physics
