雷诺应力模型的初步应用

针对SSG/LRR-ω雷诺应力模型,选取NASA湍流资源网站上的四个典型算例,即湍流平板边界层流动、带凸起管道流动、翼型尾迹区流动和NACA0012不同攻角绕流,开展初步的验证与确认工作,将部分结果和CFL3D进行对比。对于NACA0012翼型绕流,对比雷诺应力模型和SA模型的升力系数,结果表明:在失速攻角附近,雷诺应力模型明显优于SA模型。在此基础上,将该模型应用于DLR-F6翼身组合体的数值模拟,计算得到的机翼表面典型站位压力分布和实验值吻合良好,同时该模型捕捉到翼身交汇位置的小范围分离。     

微波加热辅助多孔介质水合物制样方法与装置

针对多孔介质中人工合成水合物分布不均匀问题,提出采用微波加热法制备多孔介质水合物样品的新途径,并设计了专用微波加热装置。基于电磁场理论及微波加热均匀性影响因素分析,设计了多馈源可调式波导加热系统。通过数值模拟和加热试验分析馈能口与样品间相对位置变化对装置加热均匀性影响,探讨该装置用于水合物样品制备的可行性。结果表明:装置加热均匀性受馈能口与样品间相对位置影响较大,其加热均匀性随二者间距的增加而显著提高,数值模拟与试验结果取得了较好的一致性;加热时间对装置的加热均匀性影响较小,该微波加热装置可满足制备均匀分布水合物样品的要求,同时对于其他对加热均匀性有一定要求的试验装置的设计具有参考意义。     

可执行体系结构研究

体系结构是系统设计与实施的蓝图,它能否正确、合理地指导实践在很大程度上依赖于体系结构的验证与评估.可执行体系结构研究为体系结构验证与评估开辟了新的途径.为了使各体系结构产品在整体上形成一个执行体,提出了可执行体系结构执行规则描述这一个概念.执行规则描述体系结构产品的执行、调用与数据流关系,为体系结构的执行提供了特定的背景信息.它通过标准的动态可执行模型接口分别调用该模型的执行引擎,从而达到体系结构在整体上执行的目的.体系结构的正确执行为体系结构验证提供依据,同时其运行结果为体系结构的评估提供依据.     

YHFT-DX处理器全定制EDA技术的开发与应用

在YHFT-DX处理器的研制中,研究并实现了多项支撑全定制设计的EDA技术。针对全定制设计的功能验证,研究并实现了层次式功能模型自动提取技术,能够将晶体管级网表转化为等效的RTL级网表。研究并实现了晶体管级混合时序分析方法,可自动分析全定制设计的延时,并采用多线程并行的方法获得了约10倍左右的速度提升。为提高模拟结果分析的效率,开发了一个延时提取的工具Aimeasure。开发了两个信号完整性分析工具PNVisual和NoiseSpy,分别用于全定制设计的IR-Drop分析和噪声分析。上述技术已在YHFT-DX处理器的设计中得到了广泛应用,有效提高了全定制设计的效率与质量。     

FACILITATING NUCLEAR DISARMAMENT: Verified Declarations of Fissile Material Stocks and Production

Unprecedented interest in seeking progress toward nuclear disarmament exists today; even some nuclear weapon states are looking for new ways to strengthen this process. National declarations of fissile material holdings—highly enriched uranium and plutonium—could play an important role in supporting this effort, facilitating not only transparency but also the irreversibility of the process. This article discusses what kind of content such declarations could have in order to be meaningful and effective, the sequence of data on fissile material holdings that states might release, and some of the challenges to be expected in reconstructing historic fissile material production; it also summarizes current attitudes of weapon states toward making such declarations. Initial declarations can be valuable as confidence-building measures, but better and more background data are necessary if declarations are to serve as the groundwork for deeper cuts in the nuclear arsenals. A robust verification approach would ultimately require inspectors to have access to fissile material production and storage sites. The methods and tools of nuclear forensic analysis—in this context also dubbed nuclear archaeology—would be a key element of this process. This article discusses the capabilities and limitations of potential approaches to verifying declarations of historic production of plutonium and highly enriched uranium; it also identifies and discusses opportunities for further research and development.     

GETTING BETTER ALL THE TIME

Detect and Deter: Can Countries Verify the Nuclear Test Ban?, by Ola Dahlman, Jenifer Mackby, Svein Mykkeltveit, and Hein Haak. Springer, 2011. 279 pages, $129.     

求解布尔不可满足子式的消解悖论算法

求解布尔不可满足子式在超大规模集成电路设计与验证领域都具有非常重要的理论与应用价值,帮助EDA工具迅速定位错误与不一致。针对求解不可满足子式的非完全方法,提出了消解悖论与悖论解析树的概念,在此基础上提出一种启发式局部搜索算法。该算法根据公式的消解规则,采用局部搜索过程直接构造证明不可满足性的悖论解析树,而后递归搜索得到不可满足子式;算法中融合了布尔推理技术、动态剪枝方法及蕴含消除方法以提高搜索效率。基于随机测试集进行了实验对比,结果表明提出的算法优于同类算法。     

空间引力波探测无拖曳技术现状与趋势

航天器无拖曳控制是实现引力波空间探测科学平台超静超稳运行的核心关键技术之一。目前,国内外各研究机构对航天器系统的动力学与控制进行了深入研究,并针对不同的探测频段需求提出了不同的探测任务。根据探测任务进行了航天器编队设计与控制的详细介绍和分析,对涉及的无拖曳与姿态控制、高精度惯性传感器与执行机构等原理和理论方法进行了深入的剖析。针对现已开展的空间引力波探测无拖曳航天器在轨飞行的演示验证整体情况进行详述和分析。在此基础上,提出后续开展相关研究中亟待解决的关键问题,指出未来无拖曳航天器系统动力学与控制的研究热点和趋势。     

Modeling of the whole process of shock wave overpressure of free-field air explosion

The waveform of the explosion shock wave under free-field air explosion is an extremely complex problem. It is generally considered that the waveform consists of overpressure peak, positive pressure zone and negative pressure zone. Most of current practice usually considers only the positive pressure. Many empirical relations are available to predict overpressure peak, the positive pressure action time and pressure decay law. However, there are few models that can predict the whole waveform. The whole process of explosion shock wave overpressure, which was expressed as the product of the three factor functions of peak, attenuation and oscillation, was proposed in the present work. According to the principle of explosion similarity, the scaled parameters were introduced and the empirical formula was absorbed to form a mathematical model of shock wave overpressure. Parametric numerical simulations of free-field air explosions were conducted. By experimental verification of the AUTODYN numerical method and comparing the analytical and simulated curves, the model is proved to be accurate to calculate the shock wave overpressure under free-field air explosion. In addition, through the model the shock wave overpressure at different time and distance can be displayed in three dimensions. The model makes the time needed for theoretical calculation much less than that for numerical simulation.     

环境水平不变的水声环境参数盲估计与实验验证

为秘密、隐蔽地获取非常时期或非合作海区的水声环境参数,提出了水声环境参数盲估计的概念,分析和研究了水声环境参数盲估计理论,并对其中的目标函数进行了详细探讨,同时利用SWelIEx-96海试的部分数据对基于水平不变的水声环境参数盲估计方法进行了实验验证.实验结果表明,基于环境水平不变的水声环境参数盲估计技术是可行和有效的.