摘要
针对鸭翼对鸭式布局战斗机整机的雷达散射截面(RCS)影响进行了较详细的研究与分析。首先,分析了鸭翼的散射机理,然后运用多层快速多极子方法(MLFMM)进行特定模型的整机外形RCS计算,通过鸭式布局和常规布局的RCS对比,分析了鸭翼散射对整机RCS的影响,包括鸭翼偏转状态下对整机的影响。然后,通过试验方法研究了鸭翼边缘散射和对缝散射的影响以及相应的抑制措施。研究结果表明,对鸭翼散射进行抑制或消除之后,鸭式布局完全可以应用于高隐身飞机的布局设计,其隐身性能与常规布局相当。最后,总结得出鸭翼隐身设计的指导性原则。
This paper studies the Radar Cross-Section(RCS)effect on canard configuration fighter of canard.First,the scattering mechanism of canard is analyzed.And then,the Multi-Level Fast Multipole Method(MLFMM)is used to compute the configuration’s RCS of the given fighter models.And by comparing the computational results of both the canard configuration and the conventional configuration,the RCS effect of canard is analyzed,focusing on the RCS effect on fighter after the canard is rotated.In addition,a full-size parts stealth test is conducted by researching the RCS effect on fighter of both edge scattering and gap scattering and respective inhibition measures.The test results show that,after the scattering of canard is inhibited,the RCS level of canard configuration can be applied to configuration design of stealth fighter.And its stealth capacity is comparable with that of the conventional configuration.Finally,the guiding principles of canard stealth design are postulated.
作者
郭展智
陈颖闻
麻连凤
GUO Zhanzhi;CHEN Yingwen;MA Lianfeng(AVIC Chengdu Aircraft Design and Research Institute,Chengdu 610091,China)
出处
《航空学报》
EI
CAS
CSCD
北大核心
2020年第6期259-269,共11页
Acta Aeronautica et Astronautica Sinica
