钨合金的层裂强度研究

 用压缩空气炮做冲击加载装置研究一种钨合金的层裂特性,加载应力峰值为5~10 GPa,加载应力时间宽度为0.2~0.6 μs。实验用钨合金由粉末热压烧结制成,是一种均匀混合材料。它的成份重量百分比为W（90%）、Ni（6.8%）、Fe（2.7%）和Cr（0.5%）。由锰铜压阻计测量样品靶后界面应力历史表明,此种钨合金的层裂强度与拉伸应力率的平方根呈单调递增关系,与加载应力峰值无关。回收样品的金相分析结果表明,此钨合金的拉伸断裂主要发生在铁镍混合物部位,钨晶粒的穿晶断裂只占很小部分。断口上的“杯状”凹坑表明,它主要属延性断裂机制。     

Real-time displacement measurement with large range and high accuracy using sinusoidal phase modulating laser diode interferometer

To resolve the conflict of large measurement range and high accuracy in the existing real-time displacement measurement laser diode (LD) interferometers,a novel real-time displacement measurement LD interferom- etry is proposed and its measurement principle is analyzed.By use of a new phase demodulation algorithm and a new phase compensation algorithm of real-time phase unwrapping,the measurement accuracy is im- proved,and the measurement range is enlarged to a few wavelengths.In experiments,the peak-to-peak amplitude of the speaker vibration was 2361.7 nm,and the repeatability was 2.56 nm.The measurement time was less than 26μs.     

大型地面固定军事目标“反雷达整体伪装”方法研究

随着雷达分辨率的提高以及侦察技术的不断改进，单靠器材对大型地面固定军事目标进行伪装，已经不能满足现代战争的需要，必须充分考虑目标、背景、方位物以及伪装器材性能之间的关系，提出新的方法与策略，对伪装器材进行最优化配备与设置，达到目标与背景之间的充分融合．尤其对于伪装像机场、油库这样的大型地面固定军事目标，暴露征候明显、目标集中、体积庞大、背景单一，必须从“目标群”的角度出发，结合具体的背景进行“反雷达整体伪装”．     

A Direct Comparison between Static and Dynamic Melting Temperature Determinations below 100 GPa

A preliminary experiment of sound velocity measurements for porous iron with initial average density of 6.275 g/cm^3 has been performed at pressures below 100 CPa, in order to clarify a long-standing problem that the static melting temperature Tin, mostly below 100CPa due to its technical limitations, is notably lower than the extrapolated melting data inferred from the shock wave experiments made above 200 CPa, for the sake of making a direct comparison between the experimental static and dynamic melting temperatures in the same pressure region. With the lately proposed Hugoniot sound velocity data analysis technique [Chin. Phys. Left. 22 (2005) 863], the results deduced from this Hugoniot sound velocity measurement is Tm = 3200 K at 87 CPa and Tm = 3080 K at 80 GPa, which are in good agreement with the two latest static data of Tm = 3510 K at 105 GPa and Tm = 2750 K at 58 GPa, which utilized modern improved double-side laser heating and in situ accurate x-ray diffraction techniques in experiments. It can be concluded that consensus Tm data would be obtained from static and shock wave experiments in the case that the recently improved techniques are adopted in investigations.     

高温气冷堆堆芯中子时空动力学模拟计算

研究开发三维圆柱几何堆芯多群中子时空动力学改进准静态方法模拟计算程序.对给定的模块式高温气冷堆模型进行模拟计算.初始状态下,计算结果与中子扩散程序CITATION吻合很好.动态情况下,模拟堆芯反应性、堆内各能群中子平均注量率和堆芯相对功率等物理量随时间变化,计算结果与理论分析一致.     

12MeV直线感应加速器二极管优化设计研究

 本文用MAGIC程序对设计的多种12MV直线感应加速器的二极管结构进行模拟计算,得出了二极管阴极表面电场强度分布,并根据实验研究结果,得到了结构最佳设计的二极管模型;随后利用扫描电镜方法对不同天鹅绒的结构进行了分析与发射性能实验研究。最后得到优化后的二极管产生的电子束束流参数为发射束流I_e=8.50kA,传输束流I₈=3.0kA ,打靶束流I₀=2.30kA。     

混沌神经网络的控制

提出了一种针对混沌神经网络的钉扎控制方法.利用此方法对混沌神经网络进行控制,使网络的输出稳定在网络的一个存储的模式上.实现了混沌神经网络的信息搜索,并对影响混沌神经网络控制效果的几个因素进行了讨论. 关键词： 混沌控制 混沌神经网络 钉扎控制方法     

摆动水翼的推力与流场结构数值研究

在一定的Reynolds数范围内,水生动物和微型仿生机械通常采用摆动的方式获得推力,这种摆动可以用行进波来表示,行进波的波长则描述了摆动生物的柔性．该文用浸入边界方法模拟了低Reynolds数情况下,水翼NACA-65-010在水中摆动时的流场．结果表明,水翼摆动产生推力的大小与行进波波长密切相关,随着波长的增大,推力系数减小,推进效率则在一定的波长值达到最大;推力的产生与两种流场结构有关:即反Krmn涡街和涡对,摆动水翼后缘尾迹中形成反Krmn涡街时产生的推力要大于尾迹中形成涡对产生时的推力．     

非水介质中合成介孔分子筛MCM-41

首次采用十六烷基三甲基溴化铵为模板剂、正硅酸乙酯为硅源, 分别使用无机和有机弱碱, 溶剂热晶化法在非水甘油介质中合成了介孔分子筛MCM-41, 通过XRD, N₂吸附-脱附, TG-DTG, IR, SEM等测试手段对样品进行了表征分析, 结果表明在甘油体系中得到的样品具有优良的孔结构性质. 相比于氢氧化钠, 以有机弱碱(无水乙二胺、三乙胺)作为碱源, 可以得到有序性更好、结晶度高的样品, 样品具有较窄的孔径分布.