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作 者:张乐[1] 周洲[2] 许晓平[2] ZHANG Le;ZHOU Zhou;XU Xiaoping(Institute of Systems Engineering,China Academy of Engineering Physics,Mianyang Sichuan 621900,China;School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China)
机构地区:[1]中国工程物理研究院总体工程研究所,四川绵阳621900 [2]西北工业大学航空学院,西安710072
出 处:《航空动力学报》2018年第7期1612-1621,共10页Journal of Aerospace Power
基 金:国家自然科学基金(11302178);国家预研项目(513250101)
摘 要:基于飞翼无人机(UAV)保形进气道和工程应用实例,进行了不同格栅间距的格栅设计。结合多层快速多极子方法(MLFMM)和混合网格计算方法,开展了保形进口格栅气动和隐身综合特性研究。结果表明:(1)随着格栅尺寸(间距)减小,格栅隐身效果逐渐增强;频率为1GHz下,格栅间距为波长的1/3时,格栅电磁屏蔽效率约为48.93%,而当格栅间距达到波长的1/6时,接近于完全屏蔽;(2)保形进口格栅对无人机翼面上流动干扰较小而对进气道内流特性影响明显;(3)随着格栅尺寸减小,全机升阻特性逐渐略微下降,进气道出口截面总压恢复逐渐降低而畸变指数逐渐增大。Based on the conformal inlet of flying wing unmanned aerial vehicle(UAV)and the relevant engineering application,grilles with different grille hole spacing were designed.Research on the integrated design of aerodynamic and stealthy performance was carried out based on multilevel fast multipole method(MLFMM)and the numerical simulation with hybrid grid.Results indicated:(1)With the decrease of grille hole spacing,the electromagnetic shielding effectiveness increased gradually;at the frequency of 1GHz,the electromagnetic shielding effectiveness can reach to about 48.93% when the grille hole spacing was λ/3(λrepresents wavelength),and it would be shielded entirely while the grille hole spacing reachedλ/6;(2)The conformal inlet grille generated a little influence on the fluid flow of wing surface of the flying wing UAV,but it had greater influence on the internal flow of inlet;(3)With the decrease of grille hole spacing,the lift/drag characteristic of flying wingUAV declined appreciably,while the total pressure recovery coefficient decreased and the distortion coefficient increased.
关 键 词:飞翼无人机(UAV) 保形进气道 格栅 电磁屏蔽效率 气动 隐身
分 类 号:V211.3[航空宇航科学与技术—航空宇航推进理论与工程]
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