Monte-Carlo simulation of surface crack growth rate for offshore structural steel E36-Z35

The Monte- Carlo method is used to simulate the surface fatigue crack growth rate for offshore structural steel E36-Z35, and to determine the distributions and relevance of the parameters in the Paris equation. By this method, the time and cost of fatigue crack propagation testing can be reduced. The application of the method is demonstrated by use of four sets of fatigue crack propagation data for offshore structural steel E36-Z35. A comparison of the test data with the theoretical prediction for surface crack growth rate shows the application of the simulation method to the fatigue crack propagation tests is successful.

剪切水气界面下湍流特性的实验测量

通过实验研究了受气流剪切但无明显波动的水气界面下的湍流特性。当界面剪切较强(‰≥O．20cn∥s)时，水面边界层中平均流速、速度脉动强度和Reynolds切应力的分布形状与固壁湍流相似，预示剪切水气界面和固壁附近的湍流相干结构是相类似的。另一方面，水面湍流也表现出不同于固壁湍流的细节特征。与自由面湍流不同的是，在靠近剪切水气界面的流场中流向和垂向速度脉动同时受到抑制。

Formation Of Dendritic Nanostructures In Pyrex Glass Anodically Bonded To Silicon Coated With An Aluminum Thin Film

Anodic bonding with thin films of metal or alloy as an intermediate layer, finds increasing applications in micro/nanoelectromechanical systems. At the bonding temperature of 350 degrees C, voltage of 400 V, and 30 min duration, the anodic bonding is completed between Pyrex glass and crystalline silicon coated with an aluminum thin film with a thickness comprised between 50 and 230 nm. Sodium-depleted layers and dendritic nanostructures were observed in Pyrex 7740 glass adjacent to the bonding interface. The sodium depletion width does not increase remarkably with the thickness of aluminum film. The dendritic nanostructures result from aluminum diffusion into the Pyrex glass. This experimental research is expected to enhance the understanding of how the depletion layer and dendritic nanostructures affect the quality of anodic bonding. (C) 2007 Elsevier B.V. All rights reserved.

抽油杆裂纹扩展的实验研究和剩余疲劳寿命的预测

应用超声波探测抽油杆疲劳裂纹扩展时的深度a, 通过室内实验找出D级抽油杆裂纹深度a和裂纹宽度c之间的比趋向于0.78, 简化后可直接研究超声波信号V和裂纹深度a之间的关系, 从而用V-a关系估算有疲劳裂纹D级抽油杆的剩余寿命, 避免杆断带来的经济损失.

短时微重力条件下燃料电池性能实验研究

开展了不同重力情况下燃料电池性能的实验研究.利用微重力落塔,对常重力和微重力条件下燃料电池发电时其内部的两相流动开展了可视化现场观测.对重力因素对燃料电池内部传质过程的影响进行了分析和讨论.实验结果表明:当电流密度较大时,在微重力环境中燃料电池性能较常重力环境中的有较明显下降.由于微重力条件下浮升力的消失导致气体不能及时从流道中排出,进而对直接甲醇燃料电池内的传质过程产生负面影响.

纳米铜团簇扩散性质研究

本文通过分子动力学模拟研究了纳米铜团簇的自扩散性质,结果表明Nc8949铜团簇自扩散系数随温度的升高而增大,在温度为1000 K时纳米铜团簇的扩散系数随团簇半径的倒数基本呈线性增加.同时指出在常温下团簇几乎无扩散行为,而某些文献中关于常温下晶粒扩散分子动力学模拟结果是模拟体系宏观转动造成的虚假现象.

第24届国际激波学术会议简介

国际激波学术会议（International Symposium on Shock Waves,ISSW）是国际上激波研究领域的重要系列学术会议.从1957年第一届会议在美国波士顿召开起,每隔两年召开一次,至今已召开24次.

Performance of a small high-speed liquid jet apparatus

The performance of a small high-speed liquid jet apparatus is described. Water jets of 200m/s to 700m/s have been obtained by firing a deformable lead slug from an air rifle into a stainless steel nozzle containing water sealed with a rubber diaphragm. Nozzle devices of using the impact extrusion (IE) method and cumulation (CU) method are designed to generate jets. The injection sequences are visualized using schlieren photography. The difference between the IE and CU methods in the jet generation is found.

Formation of dendritic nanostructures in Pyrex glass anodically bonded to silicon coated with an aluminum thin film

Anodic bonding with thin films of metal or alloy as an intermediate layer, finds increasing applications in micro/nanoelectromechanical systems. At the bonding temperature of 350 degrees C, voltage of 400 V, and 30 min duration, the anodic bonding is completed between Pyrex glass and crystalline silicon coated with an aluminum thin film with a thickness comprised between 50 and 230 nm. Sodium-depleted layers and dendritic nanostructures were observed in Pyrex 7740 glass adjacent to the bonding interface. The sodium depletion width does not increase remarkably with the thickness of aluminum film. The dendritic nanostructures result from aluminum diffusion into the Pyrex glass. This experimental research is expected to enhance the understanding of how the depletion layer and dendritic nanostructures affect the quality of anodic bonding. (C) 2007 Elsevier B.V. All rights reserved.

基于CFD分析的弧形翼导弹气动外形优化

为探索将高精度CFD分析引入高超声速飞行器气动外形优化设计的可行性,以6°飞行攻角、6马赫飞行速度下的最大升阻比为目标,引入CFD分析计算气动性能,使用Nelder-Mead可变多面体搜索方法对高超声速弧形翼导弹进行了气动外形优化.计算结果表明,在满足弹翼安全性的条件下,优化外形比初始外形的升阻比有明显提高(约9.22%),同时阻力系数、弹翼展长和弹翼面积均有不同程度的降低.计算结果充分证明了优化设计的有效性和采用CFD分析的必要性.依据该文结果提出一种前掠弧形翼高超声速导弹气动布局方案.

高压深层裂缝性油气藏中不定常渗流的数值研究

根据实验结果和裂缝性压力敏感地层的特性,建立了适合于不同外边界条件下裂缝性压力敏感地层的不定常渗流模型.推导出了裂缝性压力敏感地层的不定常渗流模型的有限元方程.在对区域进行非结构化网格自动划分的基础上,利用有限元计算方法计算出了无限大地层、圆形有界地层以及线性组合边界地层的裂缝性压力敏感地层的井底压力的理论曲线,并对理论曲线特征进行了分析和对比.确定了压力敏感系数以及有效井径组合参数对理论曲线的影响,得到了确定压力敏感油气藏的地层参数的方法.通过某气田高温高压深层气井的实例分析,得到了较好的分析结果,同时也验证该文所建立的裂缝性压力敏感地层的不定常渗流模型的正确性.

激光光束实时监测与自动准直系统设计

设计了一个激光光斑实时监测与光路自动准直装置,能够实时监测激光光斑并自动准直激光输出方向。基于透镜成像原理,使用CCD探测器获得光斑的二维成像,并根据两点确定一条直线原理和使用压电陶瓷电动调整架实现光路自动准直;监测控制程序采用虚拟仪器开发软件Lab View编写,可以实时监测激光光斑模式与光斑位置抖动情况,并进行反馈控制。经测试,设计装置的调整精度达0.5μrad,反馈控制频率约1 Hz,完全可降低或消除抖动周期在1 s以上的光斑飘移。

基于人工神经网络的大量程光纤实时距离干涉测量仪

提出了一种基于人工神经网络的全光纤化大量程实时距离干涉测量仪．采用双正弦相位调制方法，即通过同时调制半导体激光器的波长和干涉仪的光程差实现外差测量。为了扩大干涉仪的测量范围和消除输出信号中的交叉敏感，采用人工神经网络进行信号处理，把两路经过初步解调的干涉信号作为输入样本，物体距离的实际值作为输出样本，对神经网络进行训练，以使其具有良好的推广能力．实验结果表明神经网络的使用不仅扩大了距离的测量范围而且提高了测量精度．