Validation of full cavitation model in cryogenic fluids

Numerical simulation of cavitation in cryogenic fluids is important in improving the stable operation of the propulsion system in liquid-fuel rocket. It also represents a broader class of problems where the fluid is operating close to its critical point and the thermal effects of cavitation are pronounced. The present article focuses on simulating cryogenic cavitation by implementing the “full cavitation model”, coupled with energy equation, in conjunction with iterative update of the real fluid properties at local temperatures. Steady state computations are then conducted on hydrofoil and ogive in liquid nitrogen and hydrogen respectively, based on which we explore the mechanism of cavitation with thermal effects. Comprehensive comparisons between the simulation results and experimental data as well as previous computations by other researchers validate the full cavitation model in cryogenic fluids. The sensitivity of cavity length to cavitation number is also examined. Supported by the National Natural Science Foundation of China (Grant No. 50706042)     

Experimental investigation on the flow structure over a simplified Papilio Ulysses model

The aerodynamic characteristics of butterflies, especially those which can migrate overseas, have received a great deal of attention because they have larger-scale wingspans and lower flapping frequencies than other insects such as drosophilae and bees. The objective of this work is to investi-gate the flow structures over a simplified model of Papilio Ulysses, one kind of migratory butterflies, through hydrogen bubble visualizations, and leading-edge vortices, wing-tip vortices, separation bub-bles and horseshoe vortex wake are observed. Moreover, the variations of these structures with the angle of attack are discussed in detail. A new type of leading-edge vortices which resembles the in- versed Chinese character “八” is observed in the experiment.     

Random testing for system-level functional verification of system-on-chip

In order to deal with the limitations during the register transfer level verification, a new functional verification method based on the random testing for the system-level of system-on-chip is proposed. The validity of this method is proven theoretically. Specifically, testcases are generated according to many approaches of randomization. Moreover, the testbench for the system-level verification according to the proposed method is designed by using advanced modeling language. Therefore, under the circumstances that the testbench generates testcases quickly, the hardware/software co-simulation and co-verification can be implemented and the hardware/software partitioning planning can be evaluated easily. The comparison method is put to use in the evaluation approach of the testing validity. The evaluation result indicates that the efficiency of the partition testing is better than that of the random testing only when one or more subdomains are covered over with the area of errors, although the efficiency of the random testing is generally better than that of the partition testing. The experimental result indicates that this method has a good performance in the functional coverage and the cost of testing and can discover the functional errors as soon as possible.     

纳米压痕法测量纳米晶金属Cu薄膜力学性能的研究

采用纳米压痕法测量了不同厚度（180～1000nm）的纳米晶Cu膜的硬度和弹性模量.结果表明,Cu膜硬度与厚度的关系类似于Hall-Petch关系,而弹性模量与厚度无关,其值相比块体粗晶Cu下降了约20%,分析位移-载荷曲线发现晶粒尺寸越大的Cu膜其位移跳跃现象越明显.另外,对于不同厚度的Cu膜其临界剪切应力的范围约在3.02～4.07GPa之间,基本接近粗晶Cu的理论剪切强度,位错塞积依然是其塑性变形的主要机制.     

斜拉索辅助索减振的性能分析与试验研究

为了提高斜拉索辅助索的减振性能,分别采用辅助索阻尼器,辅助索索端阻尼器及主索索端阻尼器进行有限元及理论分析并用试验检验.有限元模型为一主跨1.4km斜拉桥的1/4索面,由38根斜拉索和4根辅助索组成.用ANSYS进行时程分析,忽略拉索内在阻尼,用MATLAB对数据进行处理.结果表明:阻尼器变形越大越能获得较大的最优模态对数衰减率;3种阻尼器均可使索网前3阶对数衰减率达到0.04,且安全系数达到2以上;主索索端阻尼器与辅助索索端阻尼器分别为最优阻尼共同作用时,减振效果不为二者单独作用之和,且低于辅助索索端阻尼器单独作用时的减振能力;辅助索索端阻尼器或主索索端阻尼器与辅助索阻尼器分别为最优阻尼共同作用时,减振效果约为二者单独作用之和.试验模型有3根主索和1根辅助索组成.试验结果证实有限元分析结果正确,二者的对数衰减率随阻尼器阻尼变化趋势相同.     

基于二阶锥规划的峰值旁瓣抑制滤波器设计

针对相位编码信号的高旁瓣问题,提出一种基于二阶锥规化的峰值旁瓣抑制滤波器设计方法。将最大增益处理损失约束下的最小峰值旁瓣滤波器设计转化为二阶锥规化问题,采用内点法进行高效求解。与已有方法相比,所提方法可以兼顾峰值旁瓣、处理增益损失和滤波器长度三方面的指标,具有设计灵活、精度高和收敛性好的优点。最后仿真和实测数据结果验证了方法的有效性。     

一种微弧氧化逆变电源控制系统

为满足微弧氧化工艺要求,设计出一种两级逆变式微弧氧化电源,介绍了该电源的控制系统.它以高性能DSP作为控制核心,通过调节输出两组4路PWM (脉宽调制)信号分别驱动前级功率逆变电路和后级斩波逆变电路.功率逆变电路采用有限双极性的控制方式以实现电压的调节,通过控制斩波逆变电路可以得到所需的各种电压波形.同时,该电源控制系统还具有过流、过欠压、过热、参数超限等故障诊断与保护功能.试验结果表明,该控制系统可以实现精密、稳定的电源控制,提高电源的适应能力.     

哈尔滨市城市边缘区环境灾害和环境风险探讨

通过对哈尔滨城市边缘区土地利用状况和工业布局的调查,分析出可能出现的环境灾害,对其潜在的环境风险进行定性的评价.同时针对边缘区生态环境现状提出相应的防治对策,为哈尔滨城市边缘区生态环境管理提供可行性建议.研究表明：哈尔滨城市边缘区的环境灾害类型主要有环境污染灾害、生态破坏灾害和突发性灾害,其中环境污染灾害的环境风险最大,如不及时采取相应防治措施,日后将对边缘区乃至整个城区生态环境造成较大危害.     

磁选铁尾砂选锌小型试验研究

尾矿的再利用越来越引起人们的重视,这是因为尾矿既是丰富的二次资源,又是潜在的、严重的环境污染源,再回收其中的有用成分是对日益减少的矿产资源的重要补充,利用不好又会给社会带来沉重的负担,文章阐述了磁选铁尾矿再选回收金属锌的试验研究.     

天堂鸟翼凤蝶平板模型绕流特性实验研究

蝴蝶的扑翼飞行因其相对翼展较大、扑翼频率低等特点引起广泛关注, 尤其是具有越 洋迁徙特性的蝴蝶更是备受瞩目. 本文以天堂鸟翼凤蝶这种长距离迁徙蝴蝶作为研究对象, 设计了简化模型, 应用氢气泡流动显示的方法研究该蝴蝶翼面绕流结构, 包括前缘涡、翼尖涡、翼身相交处的分离泡和马蹄形尾迹等流动结构, 并进一步讨论了各绕流结构随迎角的变化规律. 特别是在本实验条件下观测到的倒八字形前缘涡结构, 是一种新的流动现象.