电磁混响室高强度辐射场下机载电台敏感度研究

机载电台作为飞机典型用频机载设备,对其进行高强度辐射场(HIRF)辐照效应试验研究具有重要意 义。为了解决混响室高强度辐射场环境的快速构建、快速调控及机载设备敏感度有效测试问题,依托混响室高 强度辐射场辐射敏感度测试系统,以某型直升机机载电台为试验对象,在400 MHz~2GHz频段内,通过改变 混响室内部场强,分别确定混响室连续与步进两种工作模式下机载电台的典型故障类型和敏感度阈值。结果 表明:在试验环境场强相同的条件下,相比步进工作模式,连续工作模式更容易测试出机载电台的敏感度阈值; 搅拌器连续工作模式下,搅拌速度越快测试得到的机载电台敏感度阈值越低,随脉冲波脉宽的增加其敏感度阈 值的测试结果呈下降趋势。     

基于双机身和斜拉杆的大展弦比无人机机翼弯矩减小措施

为了减小临近空间大展弦比无人机机翼的弯矩和挠度,采用双机身和斜拉杆两种方案,对弯矩和挠度沿展向的分布进行计算与分析;同时还对斜拉杆方案下机翼受压力时的失稳特性进行研究.结果表明：两种方案均可较大程度地减小机翼弯矩和挠度;双机身方案可使最大弯矩减小为原来的24％,斜拉杆方案可使最大弯矩减小为原来的20％;且采用斜拉杆方案,在给定参数下机翼不会发生失稳现象.     

Statistical study of radio drifting pulsation structures with associated CMEs and other observations

Solar radio burst, especially the fine structures (FSs) and the drifting pulsation structures (DPSs), may be used as an important diagnostics tool to draw the evolution map of the flare loop in the initial phase of solar flares. In this work, 52 radio events were found accompanying with DPSs. They were all observed with the Solar Radio Spectrometers (0.625–7.6 GHz) of China during 1998–2004. Combining the radio observations with LASCO-C2, Goes-8 SXR, H_α, EUV and Trace observations, we analyzed all these events and obtained some statistic conclusions: First, 88% DPSs take place at the initial phase of the radio burst, and their rich spectrum characteristics are helpful to understand the events further. Second, 83% DPSs are associated with CMEs or ejection events, and all the events are accompanied by Goes SXR flare. Third, for CMEs and DPSs, which take the first step, there is no significant predominance of either of them. The relationship between the DPSs and CMEs is still not clear in this study because of the lack of spatial resolution in the centimeter–decimeter band. However, the EIT or Trace ejection happened during the onset/end time of DPSs. They are signatures of the initial phase of CMEs. Two events will be illustrated to explain this.     

民航VHF地空通信干扰对策研究

民航VHF地空通信干扰是近年来困扰中国民航的难点问题。通过对中国某机场干扰情况的深入调查和研究,明确了主要干扰源及其产生机理。同时结合中国电磁环境的实际情况和民航自身的特点,提出了从民航自身入手、加强管理、建立监控体系和应急VHF通信接收系统的解决思路。     

On the origin of cosmic rays in the spiral galaxy NGC 3310

The problem of cosmic ray production in the spiral galaxy NGC 3310 is addressed by analysing and comparing optical and radio continuum data. Tentative results indicate that on global scales relativistic electrons may be produced in the shock front associated with teh density wave while on local scales extreme population I objects may be producing them. It is inferred that the same conclusions apply to all cosmic rays produced in the disk.     

大展弦比机翼低速静气动弹性模型的设计、制作和风洞试验

通过弹性相似模型的风洞试验研究大展弦比机翼在弹性变形下的气动特性是研究飞机静气动弹性特性的重要手段。发展了一种静气动弹性模型低速风洞试验技术,针对某大展弦比机翼,设计、制作了缩比弹性结构相似模型,在南京航空航天大学NH03风洞进行了低速静气动特性风洞试验。详细介绍了弹性模型的各项技术和风洞试验结果,结果表明该项技术适合大展弦比机翼静气动弹性特性的研究,试验结果可作为大展弦比机翼设计的重要参考。     

A review of bird-like flapping wing with high aspect ratio

Bird-like flapping-wing vehicles with a high aspect ratio have the potential to fulfill missions given to micro air vehicles, such as high-altitude reconnaissance, surveillance, rescue, and bird group guidance, due to their good loading and long endurance capacities. Biologists and aeronautical researchers have explored the mystery of avian flight and made efforts to reproduce flapping flight in bioinspired aircraft for decades. However, the cognitive depth from theory to practice is still very limited. The mechanism of generating sufficient lift and thrust during avian flight is still not fully understood. Moving wings with unique biological structures such as feathers make modeling, simulation, experimentation, and analysis much more difficult. This paper reviews the research progress on bird-like flapping wings from flight mechanisms to modeling. Commonly used numerical computing methods are briefly compared. The aeroelastic problems are also highlighted. The results of the investigation show that a leading-edge vortex can be found during avian flight. Its induction and maintenance may have a close relationship with wing configuration, kinematics and deformation. The present models of flapping wings are mainly two-dimensional airfoils or three-dimensional single root-jointed geometric plates, which still exhibit large differences from real bird wings. Aeroelasticity is encouraged to consider the nonignorable effect on aerodynamic performance due to large-scale nonlinear deformation. Introducing appropriate flexibility can improve the peak values and efficiencies of lift and thrust, but the detailed conclusions always have strong background dependence.     

大功率无线电波加热低电离层

等离子体对大功率电波的欧姆耗散会使电子温度升高,进而导致电子密度和其他等离子体参数改变,实现电离层的地面人工变态.本文基于大功率无线电波与低电离层相互作用的自洽模型,分析了不同入射条件下电离层参数的变化,主要结论如下:电离层D区是电波的主要吸收区,并且其吸收强度随入射频率的升高而降低,当入射频率为6 MHz（有效入射功率为200 MW）时电子温度的最大增幅约为520 K,电子密度最大增幅为7300 cm^-3左右;电子温度达到饱和所需时间小于电子密度的饱和时间,前者具有μs量级,后者具有ms量级;停止加热后,电子温度和密度迅速恢复到初始状态,恢复时间均小于各自的饱和时间,但量级相当;入射功率越高,电子温度和密度的增幅越大,并且饱和时间也越长,在相同入射条件下,夜晚的饱和时间要大于白天.     

风扇转子叶片防颤振设计技术

以某两级风扇为对象开展防颤振设计技术研究。风扇转子叶片设计中,选择了合适的展弦比,既考虑到气动性能水平,还考虑到结构质量和颤振稳定性。采用流固耦合能量法评估所设计风扇的各排转子叶片的颤振稳定性问题,并通过叶片厚度、三维造型、根尖弦长比等设计参数的调整消除颤振风险。研究结果表明:展弦比不应是方案设计阶段防颤设计唯一的关注参数;在叶尖跨声速的转速更容易发生颤振现象;较强的叶尖前缘激波会造成较强的流固耦合作用,形成复杂的气动功分布结构;叶片厚度和尖根弦长比等参数是改善叶片颤振风险的有效参数。      

复合材料电搭接分析

电搭接是指用金属编织线或金属片将机载设备的外壳与飞机基本结构连接起来,使两者处于一个共同的电位点。飞机上采用复合材料后,由于复合材料与金属之间电性能的差异,在GJB358-87中规定的搭接电阻值就不完全适用。本文在研究了大量国内外资料的基础上,根据国内目前的技术水平,对安装在复合材料结构上的机载设备,按不同的电搭接功能要求,提出了合适的搭接电阻值。