语音信号相空间重构中时间延迟选择的改进的平均位移法

本文在分析时间序列相空间重构中的时间延迟选取的平均位移法基础上,对该法的原有度量进行改进,得到较好的求时间延迟的准则。改进的平均位移法具有更强的理论依据;应用于语音信号相空间重构的仿真实验表明,其度量一般情况下可得到合适的时间延迟。     

三组元喷嘴混合特性的试验研究

本文对四种类型的气氢／液氧／煤油三组元喷嘴进行了混合特性试验, 研究了内喷嘴的缩进长度对同轴离心外混式喷嘴混合特性的影响, 对比了相同的三组元工况下各喷嘴的混合特性, 分析了喷嘴结构对混合特性的影响, 进行了单喷嘴和三喷嘴的混合特性试验, 试验结果表明： 在相同的三组元工况下, 同轴直流式喷嘴的流强分布跨度比同轴离心式喷嘴小。所得结论对三组元喷嘴和气液同轴式喷嘴的优化设计有参考价值。     

自适应准则的舵减横摇控制系统的仿真研究

本文根据舵减横摇系统的模型结构及控制系统的各项要求,提出了自适应控制准则,借用人工智能和模糊控制思想,将操舵系统的限定、操纵者的要求和外界环境的变化归纳为加权阵的改变上,然后根据变化后的加权阵通过求解黎卡提方程得到最优控制量Ｕ＝－Ｋ＊Ｘ,以实现最优控制。作者在计算机上对该系统进行仿真试验,得到了令人满意的结论。     

不同的扩散模型对再入体等离子体鞘电子密度分布的影响

本文研究不同的扩散模型对再入体等离子体鞘电子密度分布的影响。由于电子和离子的质量相差三个量级以上,电子的浓度扩散速度比离子大得多,引起正负电荷分离。由此产生的诱导电场又阻碍带电粒子的扩散运动。本文同时考虑这二种影响扩散的因素,得到了非平衡等离子体鞘带电粒子分布的数值解,并与准中性模型、双极扩散模型等其它三种近似模型进行了比较。计算表明:流场的大部份区域满足等离子体准中性假定,但在物面和激波附近存在电荷分离较明显的薄层,其厚度约为Debye屏蔽长度的量级。这种边界效应对中性粒子的分布影响甚微,但对带电粒子的分布则产生一定的影响。由此可以判断各种扩散模型的适用性。     

多处理机系统的微任务并行

本文讨论微任务技术及其在多机系统上的实现。微任务技术使得一个程序能在循环和语句块一级并行执行,它的显著特点是系统开销较小、效率较高,适应于小粒度并行。     

Fabrication and characterization of Al-CuO nanocomposites prepared by sol-gel method

In this study, Al-CuO nanocomposites were fabricated by sol-gel method. As a contrast, the thermite was prepared by physical mixing at the equivalence ratio of 0.5, 1, 2, respectively. The intermediates and samples as prepared were characterized by SEM and XRD. The exothermic properties of the two samples prepared at different equivalence ratios were tested and the reaction products were characterized by XRD. The SEM results show that the sample prepared by the sol-gel method demonstrates a micron-sized agglomerated sphere formed by a mutual wrapping of Al NPs and CuO NPs, and the particles are evenly distributed in the agglomerate. In addition, when the content of Al powder is seriously insufficient, the heat release of the sample prepared by physical mixing is 1.6 times that of by sol-gel method. With the increase of Al powder content, the exothermic properties of Al/CuO NPs prepared by sol-gel method began to increase significantly compared with physical mixing and the difference is 1.5 times when the equivalence ratio increases to 2. It can be concluded that the reason for this result may be attributed to the different mass transfer modes of components due to the different morphologies of samples.     

Bayesian sampling plans for exponential distributions with interval censored samples

This article studies the problem of designing Bayesian sampling plans (BSP) with interval censored samples. First, an algorithm for deriving the conventional BSP is proposed. The BSP is shown to possess some monotonicity. Based on the BSP and using the property of monotonicity, a new sampling plan modified by the curtailment procedure is proposed. The resulting curtailed Bayesian sampling plan (CBSP) can reduce the duration time of life test experiment, and it is optimal in the sense that its associated Bayes risk is smaller than the Bayes risk of the BSP if the cost of the duration time of life test experiment is considered. A numerical example to compute the Bayes risks of BSP and CBSP and related quantities is given. Also, a Monte Carlo simulation study is performed to illustrate the performance of the CBSP compared with the BSP. The simulation results demonstrate that our proposed CBSP has better performance because it has smaller risk. The CBSP is recommended. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 604–616, 2015     

Q_2黄土调整吸力的非饱和三轴压缩试验研究

通过对Q2黄土进行调整吸力的非饱和三轴压缩试验,研究了浸水湿化程度对Q2黄土力学特性的影响。试验表明:不同浸水湿化程度的Q2黄土,其应力应变曲线为弱软化型,浸水湿化程度越高,软化程度越弱,浸水湿化至饱和时可近似看作理想硬化型;轴向应变较小时,Q2黄土的天然结构保持良好,应力随应变的增大而增大,随着轴向应变进一步增大,其天然结构逐渐被破坏,应力随之先缓慢上升后逐渐减小直至稳定;浸水湿化会同时引起土体应力状态和土体结构的改变,屈服应力随浸水湿化程度的提高而减小,在浸水湿化接近饱和时屈服应力变化最快,土体结构变化最大;形成年代早的Q2黄土细粒质量分数高,结构特征区别于Q3黄土,因而呈现出不同的力学特征。     

膨润土-砂混合型缓冲／回填材料液塑限试验

为研究掺砂率对高庙子膨润土一砂混合型缓冲／回填材料液塑限的影响,利用液塑限联合测定仪进行了试验研究,并运用最小二乘法对混合物液塑限试验数据进行了分析。试验结果表明膨润土一砂混合物的可塑性、液塑限值和塑性指数均随掺砂率的增大而降低。对试验结果进行分析,得到了考虑掺砂率影响的混合物液塑限经验公式。混合物的液塑限并不是随掺砂率增大成比例降低,而是液限的实测值小于理论值,塑限的实测值大于理论值。得到的不同掺砂率的膨润土一砂混合型缓冲／回填材料液塑限试验数据可为高放废物深地质处置库建设提供科学依据。     

Controllable combustion behaviors of the laser-controlled solid propellant

Microsatellites have been widely applied in the fields of communication,remote sensing,navigation and science exploration due to its characteristics of low cost,flexible launch mode and short development period.However,conventional solid-propellant have difficulties in starting and interrupting combustion because combustion is autonomously sustained after ignition.Herein,we proposed a new type of solid-propellant named laser-controlled solid propellant,which is sensitive to laser irradiation and can be started or interrupted by switching on/off the continuous wave laser.To demonstrate the feasibility and investigate the controllable combustion behaviors under different laser on/off conditions,the combus-tion parameters including burning rate,ignition delay time and platform pressure were tested using pressure sensor,high-speed camera and thermographic camera.The results showed that the increase of laser-on or laser-off duration both will lead to the decrease of propellant combustion performance during re-ignition and re-combustion process.This is mainly attributed to the laser attenuation caused by the accumulation of combustion residue and the change of chamber ambient temperature.Simultaneously,the multiple ignition tests revealed that the increased chamber ambient temperature after combustion can make up for the energy loss of laser attenuation and expansion of chamber cavity.However,the laser-controlled combustion performance of solid propellant displayed a decrease trend with the addi-tion of ignition times.Nevertheless,the results still exhibited good laser-controlled agility of laser-controlled solid propellant and manifested its inspiring potential in many aspects of space missions.