摘要
为了降低战斗机的雷达散射截面(RCS,Radar Cross Section)特性,研究了双立尾外倾对战斗机RCS特性的影响.对战斗机的三维数字样机进行网格划分,基于物理光学法数值模拟出双立尾向两侧对等偏转对三翼面战斗机的头向、侧向和尾向的RCS特性的影响,并对战斗机的缩比实体样机进行电磁测试,证明了方法的可行性和数值模拟的准确性.数值模拟结果表明,当双立尾从0°向外偏转10°时,三翼面战斗机侧向RCS值缩减至原来的9.8%,而头向和尾向的RCS值变化幅度较小.
In order to reduce the radar cross section （RCS） of fighter, the twin-vertical-tails effect on the RCS character of fighter was studied. The 3D digital fighter prototype was meshed. The RCS character effect of head, side and tail in three-surface fighter when twin-vertical-tails had a same deflection to two direction based on physical optics method was simulated. The electromagnetic testing on prototype fighter shrunk on a certain scale was made. The practicality of the physical optics method and the accuracy of numerical simulation were verified. The simulation results show that the side RCS of three-surface fighter reduced to 9.8% of what it had been, but the head and tail RCS had a little change when twin vertical fins deflected from 0° to 10°.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
2014年第2期160-165,共6页
Journal of Beijing University of Aeronautics and Astronautics
基金
国家973基础研究资助项目(61320)
总装"十二五"预研项目
关键词
双立尾
隐身
飞机总体设计
物理光学法
twin-vertical-tails
stealth
aircraft conceptual design
physical optics method
