含表面裂纹非匹配焊接接头的断裂行为

测试了两种超高强度钢低匹配接头母材、焊缝和热影响区的表面裂纹断裂韧性,比较了母材与热影响区的断裂韧度概率分布.同时采用有限元方法分析了匹配因子和裂纹位置对裂纹尖端张开应力和应力三轴度的影响.结果表明,当裂纹位于热影响区时,由于软焊缝使其应力三轴度降低,其断裂韧性明显好于母材;而当裂纹位于焊缝一侧时,匹配因子越高,距熔合线越远,则应力三轴度越低,断裂韧性越好;当裂纹位于焊缝中心时,两种匹配的断裂韧度相当.从而解释了试验结果.     

初始啁啾对光纤中传播的飞秒光孤子的影响

采用分步傅里叶变换作为数值模拟的方法,以二阶飞秒光孤子和基态飞秒光孤子为例,讨论了初始啁啾对光纤中传播的飞秒光孤子的时域特征和频谱结构的影响,概括出如下的结论:初始啁啾通过影响飞秒光孤子谱线的红移,而对飞秒光孤子由拉曼效应引发的脉冲延迟产生较大影响,正的初始啁啾使脉冲延迟加剧,负的初始啁啾使脉冲延迟减小.     

An investigation on TCP large initial window

Transport layer implicates a position where satellite networks form one integrated component of hybrid Internet architecture in today's advance technology. However, the Internet has emerged with an important new class of applications that exhibits significant variations of transmission rate over time. Variable‐rate traffic poses a new challenge for transmission control protocol that provides congestion control, especially for applications that need to share the limited capacity of a bottleneck over a long delay Internet path (e.g. paths that include satellite links). Variable‐rate traffic can be produced by persistent transmission control protocol connections and can be impacted by the initial window at the start or during the restart of a session. Current transport research issues are identified related to larger initial window to highlight the expected performance benefits and derive the implications on the design of geostationary satellite Internet systems as the network evolves toward a next‐generation Internet. Copyright © 2013 John Wiley & Sons, Ltd.     

便携式地空导弹海上作战使用研究

分析舰船运动特性对便携式地空导弹射击的影响,建立求解导弹初始弹道运动学参量的数学模型.针对某型便携式地空导弹进行舰船平台弹道特性分析,结果表明便携式地空导弹可以在舰船平台上实施射击.     

用Hopkinson杆技术研究材料动态断裂韧性的进展

综述应用Hopkinson杆技术进行材料动态断裂韧性研究的实验方法。介绍入射波整形技术和力传感器技术在动态断裂韧性实验中的应用。简要总结动态应力强度因子的计算方法和裂纹起裂时间的确定方法。展望动态断裂韧性研究的发展趋势。     

电容器参数对最佳发射初始位置影响的研究

目前国内外电磁发射技术发展迅速,论述了电磁炮在军事上的应用,详细介绍线圈炮的工作原理与分类,并通过试验研究发射初始位置对炮口初速和相应效率的影响.     

Measurement of video initial buffer size for mobile network

To resolve the difficulty in accurately measure the length of video initial buffering queue,two video platforms,non-encrypted Youku and encrypted YouTube,were selected to research,and the video initial buffer queue length measurement method was proposed.By identifying and analyzing the characteristics of video traffic,correlating the traffic behavior with the playing state,constructing video fingerprint database,accurate measurement of queue length was realized.The experimental results show that the measurement results of the two types could be accurate to the frame,fully meeting the need to accurately evaluate the quality of the video experience.     

AGM隔膜对VRLA电池性能的影响

介绍了超细玻璃纤维隔膜（AGM）的基本性能以及不同厂家AGM隔膜在相同的极板和装配压力等情况下对所装配电池初期容量、电解液分层情况、密封反应效率、电池循环寿命等的影响。     

In Situ Artificial Hybrid SEI Layer Enabled High-Performance Prelithiated SiOx Anode for Lithium-Ion Batteries

Considered the promising anode material for next-generation high-energy lithium-ion batteries, SiO_x has been slow to commercialize due to its low initial Coulombic efficiency (ICE) and unstable solid electrolyte interface (SEI) layer, which leads to reduced full-cell energy density, short cycling lives, and poor rate performance. Herein, a novel strategy is proposed to in situ construct an artificial hybrid SEI layer consisting of LiF and Li₃Sb on a prelithiated SiO_x anode via spontaneous chemical reaction with SbF₃. In addition to the increasing ICE (94.5%), the preformed artificial SEI layer with long-term cycle stability and enhanced Li⁺ transport capability enables a remarkable improvement in capacity retention and rate capability for modified SiO_x. Furthermore, the full cell using Li(Ni_0.8Co_0.1Mn_0.1)O₂ and a pre-treated anode exhibits high ICE (86.0%) and capacity retention (86.6%) after 100 cycles at 0.5 C. This study provides a fresh insight into how to obtain stable interface on a prelithiated SiO_x anode for high energy and long lifespan lithium-ion batteries.     

自主空中加油会合过程中飞行制导律设计

针对目前自主空中加油亟需解决的会合问题,采用带有末端角约束的比例导引方法,实现了受油机导引进入加油区域,加油机采用非线性制导算法跟踪赛马场跑道线飞行,并给出了有风条件下非线性制导算法可能失效的解决办法。引入虚拟目标和虚拟加油机的概念,保持受油机和加油机在会合上的时间同步,设计了相应的速度控制器。利用Matlab/Simulink搭建仿真平台对空中加油会合制导律进行了仿真验证,仿真结果表明设计的制导律能满足自主空中加油的会合要求。