基于飞针测试仪的电子模块的测试与实现

重点讨论了飞针在线测试技术在电子模块测试中的测试与实现。介绍了飞针测试原理,阐述了电子模块飞针测试的流程以及测试中电子模块,提出了短路测试中出现的问题的解决办法,以及NOD文件的快速修改技巧,并且详细说明了飞针和针床的互补关系。飞针测试技术的使用能准确定位故障点,缩短调试周期,对批量生产的电子模块调试有重要作用。     

汇流环接触问题分析

本文结合某产品汇流环结构,从汇流环的接触电阻性能、接触副的热性能、接触应力说明导电环硬度对汇流环接触特性的影响,从导电环的疲劳磨损机制和摩擦磨损机制探讨导电环磨屑的形成,提出了按导电摩擦副的接触应力选取导电环材料强度（硬度）的方法。     

剪切模式压电光纤调制器

设计了一种基于剪切模式振荡的光纤光调制器.实验中,利用压电陶瓷控制2段对接光纤的相对截面积,在初始位置光束无损耗的全部通过,在压电陶瓷管切向形变为光纤内径r时,输出光强为零.本光纤信号调制器属于光的振幅调制器,调制度可达到100%,信噪比(SNR)约为25 dB,带宽约为200 kHz.     

比尺模型上床面切应力研究及应用

用比尺模型研究了湘江洪道刘家坝弯曲型河段的床面切应力，得出了整治工程前后床面切应力的平面分布和阻力沿程的变化。根据试验结果，从河流阻力角度对刘家坝滩整治工程进行了评论。     

泛亚C14发动机配气机构单阀系动力学分析

利用TYCON软件分别分析评价了C14配气机构中凸轮与平面挺柱之间的动力学关系、气阀落座情况、气阀弹簧各有效圈动力特性等。     

Microstructural modifications and properties of Sn-Ag-Cu solder joints induced by alloying

Slow cooling (1–3°C/sec) of Sn-Ag-Cu and Sn-Ag-Cu-X (X = Fe, Co) solder-joint specimens, made by hand soldering, simulated reflow in a surface-mount assembly to achieve similar as-solidified joint microstructures for realistic shear-strength testing, using Sn-3.5Ag (wt.%) as a baseline. Consistent with predictions from a recent Sn-Ag-Cu ternary phase-diagram study, either Sn dendrites, Ag₃Sn primary phase, or Cu₆Sn₅ primary phase were formed during solidification of joint samples made from the selected near-eutectic Sn-Ag-Cu alloys. Minor substitution of Co for Cu in Sn-3.7Ag-0.9Cu refined the joint-matrix microstructure by an apparent catalysis effect on the Cu₆Sn₅ phase, whereas Fe substitution promoted extreme refinement of the Sn-dendritic phase. Ambient-temperature shear strength was reduced by Sn dendrites in the joint microstructure, especially coarse dendrites in solute poor Sn-Ag-Cu, e.g., Sn-3.0Ag-0.5Cu, while Sn-3.7Ag-0.9Cu with Co and Fe additions have increased shear strength. At elevated (150°C) temperature, no significant difference exists between the maximum shear-strength values of all of the alloys studied.     

Plastic deformation kinetics of electrodeposited Cu foil at low and intermediate homologous temperatures

The plastic deformation kinetics of electrodeposited (EP) Cu foil (grain size d=0.6 μm) were determined at 296–448 K and compared with those for vapor-deposited (VP) foil (d=0.5 μm) tested at 77–473 K. The apparent activation volume v=kT ∂ ln for both materials exhibited a minimum at ∼350 K, and at this temperature, there occurred a marked increase in the temperature dependence of the flow stress σ. The rate-controlling mechanism in both materials at T<373 K appears to be grain boundary shear induced by dislocation pileups at the grain boundaries. The results at T=373–473 K suggest that the dislocation pileups are relieved or prevented and that either cross slip or intersection of dislocations is rate controlling with stronger support for the latter. The determination of the rate-controlling mechanism at the higher temperatures is complicated by possible changes in defect structure due to thermal annealing, and therefore, the operative mechanism corresponds to a structure that may differ from the initial, as-deposited condition.     

基于嵌套粒子群算法的多涡环微下击暴流模型参数选择方法

 提出一种使用嵌套粒子群算法,根据微下击暴流水平垂直风速最大峰值比选择多涡环微下击暴流模型参数的方法.设计了包括目标群和中间群的嵌套式粒子群结构,使用中间群寻找水平垂直最大风速,并使用目标群最终选择模型参数.用该方法计算了水平垂直风速峰值比在0.3~0.7之间的多组多涡环微下击暴流模型参数,最终生成的微下击暴流场的水平垂直风速峰值比与预设值误差的数量级在10^-4以内.     

临近空间高超音速飞行器载监视雷达技术发展研究

本文描述了临近空间高超音速飞行器的独特优点;阐述了临近空间高超音速飞行器载监视雷达的发展优势;概述了临近空间高超音速飞行器载监视雷达的发展情况;最后提出了临近空间高超音速飞行器载监视雷达的发展设想。     

导弹战术兵棋中侵彻子母弹打击机场毁伤效果裁决

基于导弹战术兵棋使用需求,运用切断点法,对侵彻子母弹打击机场毁伤效果进行了建模分析.讨论了命中概率的计算,给出了计算公式,并对打击效果裁决进行了详细的说明和分析.在此基础上,建立了打击效果裁决表.