Effect of Vortex Restructuring on Heat Transfer in an “Inverted” Flame

The papers deals with formation of vortex structures during combustion of a fuel gas–air mixture injected vertically down through a hole in a flat plate. It has been established that the shape, position, and number of vortex cells are determined by the flow rate and composition of the fuel mixture. It is shown that as the flow rate increases from the minimum critical value for which a vortex structure arises, the number of vortex cells decreases from five or six to one. A further increase in the gas flow rate leads to transition to turbulence of the combustion product flow. The presence of a vortex structure increases the critical Reynolds number at which the flow becomes turbulent. Reverse transition to the structure with an increased number of vortex cells occurs with a delay in the gas flow rate (gas discharge hysteresis). Variation in flow rate is accompanied by bifurcation of the number of vortex cells.     

Numerical study of particle dispersion in the wake of gas-particle flows past a circular cylinder using discrete vortex method

A numerical investigation on the particle dispersion in the wake of particle-laden gas flows past a circular cylinder at Reynolds number of 10⁵ is presented. In the numerical method, the Discrete Vortex Method with the diffusion velocity model is employed to calculate the unsteady gas flow fields and a Lagrangian approach is applied to track individual particles. A dispersion function is defined to represent the dispersion scale of the particle. The distributions of gas velocities and vortex blobs, the trajectories and dispersion functions as well as distributions for particles with various Stokes numbers ranging from 0.01 to 1000 are obtained. The numerical results show that: (1) very small sized particles with St = 0.01 can distribute both in the vortex core and around the vortex periphery, whereas intermediate sized particles with St = 1.0, 10 are distributed around the vortex periphery, and very large sized particles with St = 1000 do not feel the gas flow; (2) only at small Stokes number (St = 0.01, 0.1) the particles do not impact with the cylinder; (3) the particle's dispersion intensity decreases precipitously as St is increased from 0.01 to 10.     

MCU平台的嵌入式系统软件设计研究

嵌入式系统的运行需要可靠性和实时性的保证,因此良好的可靠性和实时性是嵌入式系统软件设计的重要标准。同时为了使软件系统的鲁棒性更强,嵌入式系统的设计需要一个非常好的软件架构。这里介绍了一种基于MCU平台的嵌入式系统软件架构方法。在这个方法中,事件驱动机制的引入满足了对软件架构的要求,主程序中不仅采用了优先调度机制,同时也加入了软件抗干扰措施,这些都使系统的实时性和可靠性得到了明显的提高。设计实验比较由该方法得到的软件架构与原始软件架构的实时性,得出由该方法优化后的软件架构确实具有更好的性能。     

基于FFT与STM32 MCU的涡街信号处理系统设计

该文针对涡街传感器输出信号的特点和低流速时涡街流量计测量精度受限的问题,设计了一种基于STM32芯片的数字涡街信号处理方法与系统,将涡街传感器输出信号通过低噪声前置放大电路,可采集低流速下的涡街信号,再通过频谱分析法FFT准确计算出涡街信号频率,有效提高了测量精度。     

基于Hough变换的SAR图像舰船尾迹检测方法

该文提出了一种基于Hough变换与K均值聚类检测舰船尾迹的算法。该方法通过归一化Hough变换求出原图像尾迹所在直线的平均能量值,由于原图中的尾迹往往并不规则,导致能量最大值并不是整条直线的最佳统计代表值,其周围会有一些能量次大的点出现,且形成一个由若干能量点组成的点集。该文引进了K均值聚类方法,将这些点集归类,归类后的每一类的类心能很好的代表一条尾迹,实验结果表明方法是有效的。     

不同引渠形式下深式短管进口泄流能力的试验研究

为研究红岩河水库导流泄洪洞深式短管进口引渠形式由明渠改成涵洞后对其泄洪能力的影响,对其在明渠和涵洞两种形式下分别做水工模型试验,验证其水力特性。结果表明,较明渠形式,涵洞形式下的导流泄洪洞同水位下泄流量有不同程度的减小,下泄流量减小在导流泄洪洞进口为压力流状态时表现明显,且减小值随水位的升高而变大;大坝度汛期100年一遇洪水时,试验下泄流量较设计下泄流量约小6.35%;运行期100年一遇洪水时,试验下泄流量较设计下泄流量约小6.51%;运行期2 000年一遇洪水时,试验下泄流量较设计下泄流量约小6.95%。建议在将红岩河水库导流泄洪洞深式短管进口引渠由明渠改成涵洞形式后,需关注导流泄洪洞的下泄流量减小问题,避免由于水库下泄流量不足引起的大坝安全问题。     

纵向涡发生器攻角对翅片传热性能的影响

为了提高翅片式换热器的强化传热性能,对不同攻角的纵向涡发生器的翅片区域进行了研究.采用流体仿真软件FLUENT对发生器的翅片区域建立六面体网格模型,对不同攻角的纵向涡发生器的努塞尔数、阻力因子、综合性能分别进行数值分析和对比.结果显示:随着纵向涡发生器的攻角增加,纵向涡翅片的努塞尔数增强的越来越明显,其中纵向涡发生器攻角为45°的翅片努塞尔数最大;同时随着纵向涡发生器的攻角增加,阻力因子也随之增加;带纵向涡发生器的翅片的传热效果强于不带纵向涡发生器的翅片;通过比较综合评价因子,攻角为45°的纵向涡翅片在雷诺数为2000~6000内,综合性能最好.     

一种基于MUSIC算法的涡街信号处理方法

针对涡街流量计易受管道振动和流场扰动引起噪声干扰的问题,提出了一种基于MUSIC算法的涡街信号处理方法.介绍了涡街流量计的测量原理,建立了噪声环境下的涡街信号模型,并阐述了MUSIC算法的基本原理,在此基础上,分别对多种噪声环境下的涡街信号进行仿真研究.仿真结果表明:所提的涡街信号处理方法能有效地抑制噪声,高精度地分辨频率点,对改善涡街流量计的性能有良好的效果.     

吉音水利枢纽竖井旋流泄洪洞水力特性试验研究

通过1∶30的水工模型对吉音水利枢纽竖井旋流泄洪洞的水流流态、压力分布、流量系数等水力特性进行了研究,分析了在进水口溢流堰末端增设掺气坎对进水口及竖井内流态及通气孔风速的影响。研究结果表明:在溢流堰末端增设掺气跌坎有利于减小溢流堰面的负压、防止空蚀破坏、简化进口体型设计,且有利于泄洪洞的安全运行。     

The inception cavitating flows over an axisymmetric body with a blunt head-form

The inception cavitating flows around a blunt body are studied based on flow visualizations and velocity field measurements. The main purpose of the present work is to study the incipient cavity evolution and the interplay between the inception cavitation and the local turbulent flows. A high-speed video camera is used to visualize the cavitating flow structures, and the particle image velocimetry(PIV) technique is used to measure the velocity field, the vorticity, and the Reynolds stresses under non-cavitating and inception cavitating flow conditions. It is found that the appearance of visible cavities is preceded by the formation of a cluster of micro-bubbles not attached to the body surface and in a hairpin-shaped vortex structure. During its evolution, the cavity moves downstream with a lower speed. The effect of the incipient cavity is significant on the local vortical structures but slight on the timeaveraged velocity distribution. The mean Reynolds stress distributions in the turbulent shear flow can be substantially altered by the incipient cavities. The presence of the incipient cavities can lead to the production of turbulent fluctuations.