Analysis and characterization of orientation structure of pre-oxidized PAN fibers in high magnetic fields

PAN fibers pre-oxidized at 240 ℃, 260 ℃, 280 ℃, 300 ℃ were treated in 8 T, 12 T, 16 T high magnetic fields, respectively. The experimental result implied that there were two kinds of magnetic units cyan and carbon-nitrogen heterocycle in pre-oxidized PAN fibers, and the movement of magnetic units resulted in changes of orientation structure of pre-oxidized PAN fibers in high magnetic fields. Overall orientation increased with increase of magnetic field intensity and extension of processing time, whereas change of crystalline orientation depended on magnetic field intensity and content of carbon-nitrogen heterocycle due to the competition of two magnetic units. Furthermore, magnetic fields induced the conversion from amorphous region to crystal region and improved crystalline properties of pre-oxidized PAN fibers.     

仿蝙蝠折叠扑翼机构设计与分析

基于对蝙蝠飞行方式的研究,提出了一种仿蝙蝠扑翼飞行器设计方案,并且通过单一原动件驱动,既实现了拍动和折叠的耦合协调运动,又提高了系统的单位质量功率系数.设计的对称双翼拍动机构能保证左右翅膀同步运动,为飞行器的平稳飞行提供了保证.采用凸轮机构来控制翅翼的伸展和收缩,通过调整凸轮外轮廓线和初始相位角可以控制蝙蝠翅翼的折叠状况.拍动机构和翅翼折叠机构的协调耦合,可以实现翅翼空间运行轨迹的规划.建立了翅膀拍动和折叠的数学模型,在此基础上编写了仿真程序,仿真结果达到了预期的目标.     

江垭水电站碾压混凝土重力坝的温度应力分析

为研究温度荷载对江垭水电站碾压混凝土重力坝的影响,以其非溢流坝段为研究对象,建立有限元模型,根据江垭水电站的水温、气温、坝体温度、地基温度等监测资料,计算分析了大坝运行期的温度场,研究了大坝在温度场影响下的应力变化规律.研究结果表明:温度荷载对大坝运行有较大影响,但是大坝仍满足规范设计要求;夏季持续高温时,应避免大坝在高水位下运行;冬季持续低温时,应避免大坝在低水位下运行.     

明渠扩散段急流运动特性及调控方法研究综述

依据文献分析了有限宽度水槽突然扩散、固定扩散角渐变扩散、无边界平板扩散和急流扩散4种典型明渠扩散段水流的共同流动特征.给出了有限宽度水槽突然扩散段水流宽度的沿程发展规律,以及在平底明渠急流扩散段设计时,为防止水流脱离的扩散角计算方法和突然扩展区急流扩散的边界方程;通过不同底坡比降的试验和原型资料分析,论述了陡坡扩散区水深沿程变化特点、沿程各断面横向分布规律,介绍了陡坡上水平扩散角的计算方法与扩散角最大值的存在.通过大扩散角水槽试验,发现在扩散段不同流态的过渡水流现象及稳定性不一样.上游来流为急流时,下游水跃进入扩散段就是水流失稳、主流偏转的开始;采用潜没式三角翼可以防止扩散段回流发生,提高过流均衡性.     

液压消音器的内部流场信号传输特性

对液压管路中给定的压力阶跃信号进行数学分析,得出信号在管路中传输特性;为设计液压消音器提供了数学基础。     

计及输入变量强相关性的概率潮流计算模型

利用统计学的方法,以风电场出力为例,对其大量历史数据进行相关性分析,将具有强相关性的随机变量用最小二乘进行线性拟合,并用其中一个变量的线性表达式表示,从而消去随机变量之间的强相关性,并认为余下的呈弱相关或不相关的随机变量之间相互独立,以便采用半不变量法计算概率潮流。     

多孔介质通道气液两相流型及压降特性研究

通过高速摄影仪研究多孔介质通道内气液两相流体垂直向上流动的流型,在实验参数范围内依次拍摄到泡状流、弹状流、脉冲流、雾状流4种典型流型,并总结了各种流型的特征。依据实验获得的两相流动阻力数据,分别对分相模型阻力关系式和均相模型阻力关系式进行了拟合,得到了适于实验特点的两类阻力关系式。改进后的两类模型均与实验数据实现了较好的吻合,但模型关系式定义中包含了影响阻力压降各要素的均相模型具有更高的预测精度,且该模型物理意义更加清楚,可以优先用于多孔介质通道气液两相流动的阻力计算。     

平板太阳能空气集热器热性能的实验研究

设计了一种太阳能空气集热器,对其热性能进行了实验研究。通过实验,分析了冬季3个典型日的集热效率和空气流量、进出口温度、太阳辐射强度间的关系。结果表明,出口温度随太阳辐射强度的增加而增加,集热效率随着空气流量的增大而增大。同时给出了太阳能空气集热器的效率方程。     

Modeling electric vehicle’s following behavior and numerical tests

The micro modeling for electric vehicle and its solution were investigated. A new car-following model for electric vehicle was proposed based on the existing car-following models. The impacts of the electric vehicle＇s charging electricity were studied from the numerical perspective. The numerical results show that the electric vehicle＇s charging electricity will destroy the stability of uniform flow and produce some prominent queues and these traffic phenomena are directly related to the initial headway, the distance between two adjacent charging stations and the number of charging stations. The above results can help traffic engineer to choose the position of charging station and the electric vehicle＇s driver to adjust his/her driving behavior in the traffic system with charging station.     

A novel contour design technique of super/hypersonic nozzle diverging section with sharing throat

A straightforward technique has been developed to quickly determine the wall contour of super/hypersonic nozzles working at multiply Mach number which share a common throat section.Mach number distribution along the centerline of the nozzle is specified in advance and divided into two sections,both of which are described by the b-spline function.The first section is shared by different exit Mach number nozzles.The nozzle contour is determined by the method of characteristics plus boundary layer correction.An example of this design method is employed to illustrate the technique with a computational fluid dynamics calculation.The simulation results indicate that desired Mach numbers are obtained at the nozzle exit,and the good flow quality is attained for different nozzles within δMa/Ma±0.56% in the flow core region.This technique improves the design precision of the converging-diverging nozzle,cancels waves completely,and achieves nozzles with multiple Mach number exiting which share a common throat section.