An electromagnetic wave attenuation superposition structure for thin-layer plasma

来源 :等离子体科学和技术(英文版) | 被引量 : 0次 | 上传用户:liwei20062
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
This work proposes a new plasma super-phase gradient metasurfaces(PS-PGMs)structure,owing to the limitations of the thin-layer plasma for electromagnetic wave attenuation.Based on the cross-shaped surface unit configuration,we have designed the X-band absorbing structure through the dispersion control method.By setting up the Drude dispersion model in the computer simulation technology,the designed phase gradient metasurfaces structure is superposed over the plasma,and the PS-PGMs structure is constructed.The electromagnetic scattering characteristics of the new structure have been simulated,and the reflectance measurement has been carried out to verify the absorbing effect.The results demonstrate that the attenuation effect of the new structure is superior to that of the pure plasma structure,which invokes an improved attenuation effect from the thin layer plasma,thus enhancing the feasibility of applying the plasma stealth technology to the local stealth of the strong scattering part of a combat aircraft.
其他文献
On December 18th-19th,2021,the First Asian Young Geographers Workshop was held online.Initiated by the Young Geographers Working Group of the Asian Geographical Asso-ciation(AGA-YGWG),the Workshop was jointly organized by AGA-YGWG,Young and Early Career G
期刊
大尺度薄膜结构平面天线由于轻质、超柔特点,其动力学性能参数较为复杂.为掌握其在轨结构动力学特性,基于温度-结构预应力导入方法建立了大型空间可展薄膜结构的动力学模型,分析了可展薄膜结构的动力学特性.通过建立的动力学模型,采用特征系统实现算法(ERA)对薄膜结构平面天线的模态参数在轨辨识进行研究.辨识结果与仿真分析结果对比表明,ERA方法可以有效辨识薄膜结构平面天线的低阶固有模态,为其工程化实施奠定了理论研究基础.
发动机静叶调节机构空间运动复杂,前人的研究并未涉及整机的动力学方程,运动副特性及驱动方式对调节机构动态性能的影响尚不明晰.本文通过将第一类拉格朗日方程与改进的接触模型和LuGre摩擦模型相结合,建立了考虑转动副间隙和摩擦特性的静叶调节机构动力学模型,并探究驱动方式对调节机构动态性能的影响.针对做空间转动的连杆的质量矩阵随时间不断变化这一问题,本文给出详细推导公式.将数值模拟结果与Adams仿真进行了比较,验证结果的正确性.通过对比匀速驱动、简谐驱动及梯形驱动方式表明,简谐驱动有助于减小运动过程中的阻滞力,
在主动隔振系统中,执行机构输出的主动控制力与系统隔振性能密切联系.为研究上述问题,本文通过建立优化目标函数对双层主动隔振系统进行优化来获得最优系统参数,分析优化前后双层主动隔振系统的隔振性能及主动控制力,验证优化方法的可性行.首先,从理论上研究了双层主动隔振系统在不同激励条件下的隔振性能,并分析了系统参数对主动控制力输出的影响.其次,建立综合性的优化目标评价系统的隔振性能,利用遗传算法优化目标函数.最后,利用模糊PID控制算法对双层主动隔振系统进行主动控制,对比优化前后的隔振性能及主动控制力,其结果表明:
A two-dimensional electromagnetic particle-in-cell simulation model is proposed to study the density evolution and collective stopping of electron beams in background plasmas.We show here the formation of the multi-layer structure of the relativistic elec
Based on the conventional tokamak HL-2A-like parameters and profiles,the linear properties and the nonlinear dynamics of non-resonant kink mode(NRK)and non-resonant fishbone instability(NRFB)in reversed shear tokamak plasmas are investigated by using the
在航天航空领域,增材制造板状结构因其优异特性而得到广泛应用.但是增材制造结构件在制造或者使用过程中极有可能会产生不同类型的缺陷,从而造成安全隐患.本文基于兰姆波在平板中具有多个路径的传播形式,提出了一种利用二次到达波的缺陷无损检测方法,并应用于增材制造平板的缺陷定位.首先,根据兰姆波的频散特性确定激励信号的中心频率和模式.设计兰姆波在板中的多种传播路径,通过预先设置的压电片传感器接收二次到达波.通过波速和消耗时间来计算从传感器到缺陷的距离,以传感器为中心、以测得的传感器到缺陷的距离为半径做圆,进而利用两圆
In this study,the neutral gas distribution and steady-state discharge under different discharge channel lengths were studied via numerical simulations.The results show that the channel with a length of 22 mm has the advantage of comprehensive discharge pe
刚体的构形可用其质心位置和姿态矩阵描述.刚体的位置可以在欧几里得空间中表示,但是其姿态矩阵是在李群上演化的.由于李群独特的非线性性质,基于欧氏空间的多体动力学建模与数值算法难以完全真实地描述系统的动力学特性,特别是长时间历程的动力学特性.本文基于几何力学理论,首先根据离散Ham-ilton变分原理与离散Legendre变换,建立了多刚体系统的Hamilton体系李群变分积分公式.其次,给出李群变分积分公式的两种离散格式:一般离散格式和RATTLie离散格式.最后,采用这两种不同离散格式构建的算法计算了重力
In this work,the gyrokinetic eigenvalue code LIGKA,the drift-kinetic/MHD hybrid code HMGC and the gyrokinetic full-fcode TRIMEG-GKX are employed to study the mode structure details of reversed shear Alfvén eigenmodes(RSAEs).Using the parameters from an AS