结构吸波材料多层阻抗渐变设计及应用

对多层阻抗渐变的吸波结构设计思想进行了分析,介绍了多层阻抗渐变思想在吸波层板和泡沫两类结构吸波材料设计上的应用。理论计算与试验验证结果均表明,采用多层阻抗渐变设计能够使吸波层板和泡沫的吸波带宽向低频拓展,同时显著提高吸波泡沫的吸收强度。具有三个阻抗渐变吸收层的4 mm厚吸波层板在5~18 GHz频段反射率小于-10 d B;具有六个阻抗渐变吸收层的22 mm厚吸波泡沫在2~18 GHz频段反射率小于-10 d B,其中在6~18 GHz频段反射率小于-20 d B,8~12 GHz频段反射率小于-30 d B。多层阻抗渐变设计是提高结构吸波材料吸波性能的有效手段。     

Spatio-temporal structure of the wave packets generated by the solar terminator

Using long-term (1998--2009) total electron content (TEC) measurements from the GPS global network including dense network of GPS sites in USA and Japan, we have obtained the first data regarding the spatio-temporal structure and the statistics of medium-scale traveling wave packets (MS TWPs) excited by the solar terminator (ST). Total amount of the detected TWPs exceeds 565,000. There is no correlation between TWPs occurrence and geomagnetic and solar activity. We found that the diurnal, seasonal and spectral MS TWPs characteristics are specified by the solar terminator (ST) dynamics. MS TWPs are the chains of narrow-band TEC oscillations with single packet’s duration of about 1–2 h and oscillation periods of 10–20 min. The total duration of chain is about 4–6 h. The MS TWPs spatial structure is characterized by a high degree of anisotropy and coherence at the distance of more than 10 wavelengths. Occurrence rate of daytime MS TWPs is high in winter and during equinoxes. Occurrence rate of nighttime MS TWPs has its peak in summer. These features are consistent with previous MS travelling ionosphere disturbance (TID) statistics obtained from 630-nm airglow imaging observations in Japan. In winter, MS TWPs in the northern hemisphere are observed 3–4 h after the morning ST passage. In summer, MS TWPs are detected 1.5–2 h before the evening ST appearance at the point of observations, but at the moment of the evening ST passage in the magneto-conjugate point. The obtained results are the first experimental evidence for the hypothesis of the ST-generated ion sound waves.     

基于NetLogo的终端区交通流仿真

空中交通流仿真可用于分析空中交通流特性及其要素之间的相互关系,以揭示空中交通流随时间和空间的变化规律,阐明空中交通现象及其机理。采用多智能体仿真工具NetLogo建立终端区进场交通流仿真模型,并实例化描述了工具在空中交通实验中的建模和实验过程。结果表明,基于智能体的仿真建模工具可用于空中交通仿真实验,较好地再现真实世界的交通流特性。NetLogo是一个方便实用的空中交通仿真建模研究工具。     

Estimated errors in a global gravity wave climatology from GPS radio occultation temperature profiles

In a previous paper by Schmidt et al. (2008), from CHAllenging Minisatellite Payload (CHAMP) Global Positioning System (GPS) radio occultation data, a comparison was made between a Gaussian filter applied to the “complete” temperature profile and to its “separate” tropospheric and stratospheric height intervals, for gravity wave analyses. It was found that the separate filtering method considerably reduces a wave activity artificial enhancement near the tropopause, presumably due to the isolation process of the wave component. We now propose a simple approach to estimate the uncertainty in the calculation of the mean specific wave potential energy content, due exclusively to the filtering process of vertical temperature profiles, independently of the experimental origin of the data. The approach is developed through a statistical simulation, built up from the superposition of synthetic wave perturbations. These are adjusted by a recent gravity wave (GW) climatology and temperature profiles from reanalyses. A systematic overestimation of the mean specific wave potential energy content is detected and its variability with latitude, altitude, season and averaging height interval is highlighted.     

手征媒质的手征参量ξc对反射特性的影响

利用传输线理论 ,分析金属衬底的单层手征介质与自由空间的分界面上电磁波垂直入射时 ,ξc数值的变化对媒质反射特性的影响。计算结果及部分实验结果表明 :在媒质中掺杂手征微结构的浓度增加 ,等效于ξc 的实部与虚部同时变化。分别改变ξc的实部与虚部 ,结果发现 ,手征参数ξc的虚部调整在最佳值时 ,会在某一频率点上取得最小反射率 ;而随着ξc的实部增加 ,最小反射频率减小。由此得出结论 ,在设计手征吸波媒质时 ,可以通过优化设计 ξc的实部、虚部的值 ,来实现在某一波段上较佳的吸波特性。     

镉镍电池浸渍液中镁,钾,钙含量的测定

用 原子吸收分光光度法进行镉镍电池渍液中镁，钾，钙含量的测定是一种新的先进的分析方法。介绍了镁，钾、钙各自最佳的测定条件及呈良好线性范围的浓度。     

波段探测率D_(△λ)~*替代峰值探测率D_(λp)~*的讨论

文中描述了波段探测率D_(Δλ)~*的定义和计算方法,通过对空间应用的长波红外探测器的波段探测率D_(Δλ)~*与目标辐射源温度T的关系讨论,来说明波段探测率D_(Δλ)~*(和波段响应率)替代峰值探测率D_(Δλ)~*(和峰值响应率)的优越性,文中还给出了波段探测率D_(Δλ)~*的测试方法和实验计算。     

Reduction of satellite electromagnetic scattering by carbon nanostructured multilayers

We propose a low observable satellite covered by layered materials. The dielectric properties of the composite materials are analyzed using the coaxial air-line method. Our solution could result in cost-effective applications for satellite stealthness. The particle swarm optimization algorithm is used to design and optimize layered absorbers. The obtained reflection is below −20 dB in many frequency subranges, also under an oblique incident condition, within the band 2–18 GHz. The optimized layered absorbers are used as a cloak for cube satellites. In particular, we investigated a very simple geometry by using a finite element commercial software in the band from 2 to 18. Finally, the transmission through an aperture on the satellite surface is analyzed. It is highlighted that the optimized layered absorbers attenuate the electric field within the satellite, improving its immunity against electromagnetic interferences.     

雷达吸波涂层胶粘剂的现状与发展

综述了雷达吸波涂层胶粘剂的发展概况，论述了三种综合性较好，工艺稳定的胶粘剂体系的研究现状，并对用上述三类胶粘剂所制ＲＡＣ的性能和胶粘剂的介电性能作了介绍，最后指出了在胶粘剂研究中应解决的主要问题。     

Shock/shock interactions between bodies and wings

This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supersonic flows. The body is simplified to a flat wedge and the wing is assumed to be a sharp wing. The theoretical spatial dimension reduction method, which transforms the 3D problem into a 2D one, is used to analyze the SSI between the body and wing. The temperature and pressure behind the Mach stem induced by the wing and body are obtained, and the wave configurations in the corner are determined. Numerical validations are conducted by solving the inviscid Euler equations in 3D with a Non-oscillatory and Non-free-parameters Dissipative (NND) finite difference scheme. Good agreements between the theoretical and numerical results are obtained. Additionally, the effects of the wedge angle and sweep angle on wave configurations and flow field are considered numerically and theoretically. The influences of wedge angle are significant, whereas the effects of sweep angle on wave configurations are negligible. This paper provides useful information for the design and thermal protection of aircraft in supersonic and hypersonic flows.