Study on the role of rivulet in rain–wind-induced cable vibration through wind tunnel testing

Rain–wind-induced vibration (RWIV) of stay cables has become a concern in bridge engineering over the past decades. The excitation mechanism of RWIV remains unclear. Many researchers believe that the upper rivulet is crucial to RWIV. However, experimental study on rivulet is challenging and limited. The current study designs and tests a cable model of 160 mm in diameter in an open jet wind tunnel. The upper rivulet movement and cable vibration are simultaneously measured. The importance of the upper rivulet in RWIV is directly demonstrated by alternately controlling the upper and lower rivulets. The characteristics of the upper rivulet movement and the effects of this movement on RWIV are investigated in detail. The experiment shows that the rivulet–cable system is coupled, which causes the cable and upper rivulet to vibrate at different amplitudes under the same wind speed. The upper rivulet harmonic movement changes the wind loading on the cable, causing the harmonic vibration of the cable, which in turn exerts a harmonic inertia force on the rivulet. A large vibration of the coupled system then develops.     

双目视觉技术在高超声速颤振风洞试验中的应用

以验证高超声速颤振风洞试验技术为目标,为了获取试验模型在风洞流场激励下的位移形貌,运用风洞试验的方法研究了某翼面模型的颤振特性。采用一种基于双目视觉系统的试验方法,系统主要由CCD相机、图像采集卡和控制计算机组成,通过立体视觉标定和数字图像处理技术解算出模型变形的形貌。试验结果表明,该方法应用成功,与CFD/CSD数值计算结果比对良好,验证了该技术在高超声速风洞试验中应用的可行性。     

三角形格构式塔身杆件风荷载及流动干扰特性

针对输电塔结构精细设计及优化设计对杆件风荷载准确输入的要求,选用完全结构化的多块网格,通过求解N-S方程得到了不同风向角条件下的三角形塔身节段模型流场并利用风洞试验对其体型系数进行验证．与各国规范的对比分析表明,《英国杆塔荷载规范》可用于相关设计工作;分析了不同杆件风荷载随风向角变化的成因,指出了迎风面积变化主导了最上游主材的风荷载特性,而其它两根主材的风荷载同时受到迎风面积变化及上游杆件流动干扰的影响;利用不同高度、不同展向位置的截面流线方法研究了塔身节段模型杆件之间的流动干扰性态,结果表明,如下四种流动干扰行为共同决定了节段模型的杆件风荷载特性：a）相互独立的流动干扰杆件群;b）屏蔽作用;c）两组独立的斜置阵列的流动干扰作用;d）尾迹干扰作用．     

Accuracy analysis and stabilization design of the Fabry–Perot frequency discriminator in double-edge wind lidars

The measurement error of a double-edge wind lidar caused by a disturbed Fabry–Perot interferometer (FPI) is analyzed. Several error sources such as air pressure variations, temperature changes, and mechanical vibrations are considered in the measurement-error model. The simulation results show that a double-edge wind lidar is so sensitive to environmental variations that the measurement error reaches ±60 m/s if the FPI is not stabilized. In order to compensate the external disturbance acting on the FPI, a nonlinear proportional–integral–derivative (PID) control scheme is designed based on the transmission measurement of the calibration channel. An arc tangent function is used to improve the feedback gain of the usual PID control design. The results show that with the new controller the measurement accuracy of the wind lidar can be improved 4–5 times in comparison with the usual control design, and the range of the measurement error is only ±3 m/s.     

菲佐测风激光雷达及风速反演算法

 研制了基于菲佐干涉仪的测风激光雷达系统,并使用高斯拟合法和最大似然法反演风速,对两种风速反演方法进行了分析,结果表明：风速较小时,两种方法具有相似的风速反演精度,但高斯拟合法收敛快、受条纹信噪比影响较小;风速较大时,高斯拟合法会由于条纹移出而产生较大误差,而最大似然法在处理风速较大情况时具有优势。实际风速测量时,应根据风速估计值的大小,采用两种方法分别处理大风速和小风速时的情况。最后,使用研制的测风激光雷达系统和风速反演算法,得到了1.5 km以内的大气风速廓线。     

模拟大气风场及其数据处理技术的研究

热层大气风速的测量可以采用干涉法来进行,由于光源（气辉辐射谱线）的强度很弱,故干涉法对测量系统要求很高。利用半导体激光器（LD）的调制特性和法布里-帕罗干涉仪(FPI)的高光谱分辨能力设计了一种用简单设备进行大气风场模拟与测量的方法。改变LD的驱动电流使其输出激光频率改变,从而模拟气辉辐射的多普勒频移,通过分析FPI获得的干涉图可检测出该频移,进而得到等效风速。模拟风速的相对误差不超过6.5%,最小模拟风速为20.01m/s,且测量结果与LD的线性调制特性很相符。使用该方法可以有效地对多普勒风速测量原理、数据处理方法、系统性能以及测量误差进行分析和评估。     

相干多普勒测风激光雷达

 鉴于多普勒测风激光雷达在航空航天、遥感遥测、气象观测等军事及民用领域中的广泛应用,结合相干探测工作原理,介绍了国外几种典型波段相干多普勒测风激光雷达系统,重点分析了激光发射机/接收机、空间扫描、数据处理等关键技术,并对相干多普勒激光雷达的广阔应用前景进行了展望。指出国内相干多普勒测风激光雷达研究已取得的一些重要进展。     

高架污染绕建筑对流扩散风洞实验与数值仿真

采用激光衍射瞬时浓度场测量系统和图像处理系统,对不同高架与周围建筑高度比下污染点源绕建筑对流扩散进行了风洞实验.Fluent双相耦合模型与实验进行了相互校核,得到了建筑的各个高度层面污染分布、不同高度比下的污染扩散及污染分布随时间变化的规律.不同高度比对污染对流扩散具有明显的影响,建筑各高度层面污染浓度分布也存在明显差别.当高度比较小时,污染将堆积在建筑物底层.污染分布随时间变化有助于了解污染对流扩散的时间效应.结果可以为高架与周围建筑规划提供参考与依据.     

用气轨测匀加速直线运动加速度实验的改进

本文对传统的测量方法进行了误差分析与讨论,并提出一种减少实验误差的测量方法。     

Traveling Wave Solutions to the Three-Dimensional Nonlinear Viscoelastic System

In this paper, we establish the existence of traveling wave solutions to the nonlinear three-dimensional viscoelastic system exhibiting long range memory. Under certain hypotheses, if the speed of propagation is between the speeds determined by the equilibrium and instantaneous elastic tensors, then the system has nontrivial trav- eling wave solutions. Moreover, the system has only trivial traveling wave solution in some cases.