透波隐身机翼蒙皮设计参数优化方法仿真研究  

Simulation Study on Optimization Method of Design Parameters for Transwave Stealth Wing Skin

作　　者：于天立 董文锋[1] 刘文俭 范亚 YU Tian-li;DONG Wen-feng;LIU Wen-jian;FAN Ya(Air Force Early Warning Academy,Hubei Wuhan 430019,China;Air Force Shijiazhuang Flight Academy,Hebei Shijiazhuang 050051,China)

机构地区：[1]空军预警学院,湖北武汉430019 [2]空军石家庄飞行学院,河北石家庄050051

出　　处：《现代防御技术》2022年第2期45-52,共8页Modern Defence Technology

摘　　要：为同时获得良好的气动和隐身性能,基于外形隐身技术与材料隐身技术相结合的原理,提出了一种以透波为主的机翼蒙皮设计方案;为平衡透波机翼升力与机翼电磁隐身性能之间的关系,采用一种基于代理模型的策略,对透波机翼外形几何特征参数进行了优化设计。研究结果表明,经过优化后,透波机翼在频域、空域范围内保持良好的雷达散射截面(RCS)减缩特性的同时可具备足够的升力条件。所提出的代理模型精准度高,在工程上平衡跨学科领域问题时,可作为一种有效手段。In order to obtain good aerodynamic and stealth performance at the same time,based on the principle of combining shape stealth technology with material stealth technology,a design scheme of wing skin based on wave transmission is proposed.In order to balance the relationship between the lift force and the electromagnetic stealth performance of the wave transmitting wing,a surrogate model based strategy is adopted to optimize the geometric parameters of the wave transmitting wing.The results show that after optimization,the transonic wing can maintain good RCS(radar cross section)reduction characteristics in frequency domain and spatial domain and have enough lift conditions.The proposed proxy model has high accuracy,and can be used as an effective means to balance interdisciplinary problems in engineering.

关 键 词：透波机翼 隐身 雷达散射截面(RCS) 升力 代理模型 优化 

分 类 号：V218[航空宇航科学与技术—航空宇航推进理论与工程] TP391.9[自动化与计算机技术—计算机应用技术]