风吹雪廓线的风洞实验研究

利用颗粒图像测速仪对新雪形成的风吹雪进行风洞实验研究, 给出了不同高度处雪粒粒径分布函数以及平均粒径廓线、雪粒数通量廓线的分布规律. 发现当摩阻风速大于0.5 m/s 时单宽输雪率与摩阻风速满足指数函数的关系, 小于0.5 m/s 时两者满足幂函数的关系, 总体而言, 单宽输雪率与摩阻风速呈线性关系.     

考虑湍流模型的板片空间结构风荷载下流固耦合模拟

大跨空间结构凭借其新颖的外形和较大的内部空间,已经成为常用的建筑结构.由于大跨结构刚度、质量较小,受到风荷载作用时力学响应较一般结构大,同时大跨结构附近极易出现湍流影响.本文基于显式大涡模拟(ILES)和S-A (Spalart-Allmaras)湍流模型,使用ABAQUS软件对矢跨比为1:2的空间板片结构在不同风速下的风压系数进行流固耦合(FSI)模拟.风速以及不同湍流模型对大跨板片风压系数分布的影响得到了考察,并与相关的风洞实验比较.同时对板片结构受风载的力学响应进行了分析.结果显示选用大涡模拟湍流模型和雷诺时均方程方法湍流模型的流固耦合板片空间结构模型得到的风压系数及其分布和风洞试验实测数据吻合均较好.     

一种风力机气动计算的全自由涡尾迹模型

采用全自由方式建立风力机尾流场的涡尾迹模型,引入“虚拟周期”的概念,并发展一种自适应松弛因子方法,从而改善了自由尾迹迭代的稳定性,提高了迭代收敛速度。利用建立的自由涡尾迹模型,计算了风力机叶片的尾流场结构、气动性能及叶片载荷,并与实验结果进行了对比分析。结果表明,尖速比越大,自适应松弛因子方法对缩小模型计算时间越有效;全自由涡尾迹模型能准确给出风力机尾流场的结构,包括尾迹的扩张以及叶尖涡和叶根涡的产生、发展和耗散的过程,风轮扭矩与实验数据吻合;叶片载荷分布的计算结果在低风速下与实验值基本一致,但是在大风速下差别较大,说明需要一个准确的失速模型。     

Modelling of inflow-conditions for vortex particle methods to simulate atmospheric turbulence and its induced aerodynamic admittance on line-like bluff bodies

ABSTRACT

This paper presents a novel method for the simulation of aerodynamic admittance of turbulent wind on bluff line-like structures using a pseudo 3D model of Vortex Particle Method (VPM). The method is a computationally efficient extension of the 2D VPM, where a coupled set of simulation slices accounts for the 3D nature of the oncoming wind flow. Pre-computed vortex particles are seeded in each of the parallel 2D simulation slices in order to model the turbulent velocity perturbations. Here, the modelling of the inflow seeding particles is enhanced, reducing the computational cost and allowing extendibility into quasi 3D domain. This a priori computation of the seeding vortex particles is based on modelling the atmospheric turbulence characteristics. The method is applied to simulate turbulent flow around an infinitesimally thin flat-plate, to asses its validity at the viscous-rotational boundary layer, which is important for accurate fluid-structure Interaction simulations. Furthermore, sensitivity analysis to different attributes is assessed     

环境模拟实验室中近地层风速廓线的形成研究

在环境模拟实验室中利用阻尼网对实验区形成的近地层风速廓线进行了数值模拟和实验研究.阻尼网的布置方案以变孔隙率阻尼网作为指导,选用30目和16目定孔隙率阻尼网4种不同高度的混合式布置方式.数值模拟采用Fluent软件,将结构复杂的阻尼网简化为具有一定厚度的多孔介质模型,湍流模型为标准k-\varepsilon模型.结果表明可将阻尼网作为多孔介质处理,定孔隙率阻尼网的组合可在短实验段内形成所需近地层的风速廓线,模拟值与实验值吻合良好.     

Response properties at the dynamic water/dichloroethane liquid–liquid interface

ABSTRACT

We present a novel approach for calculating the static dielectric permittivity profile of a liquid–liquid interface (LLI) from molecular dynamics simulations. To obtain well-defined features, comparable to those observed at solid–liquid interfaces, we find it essential to reference to the instantaneous liquid–liquid interface rather than the more commonly used average Gibbs interface. We provide a coarse-grained approach for the practical definition of the instantaneous interface and present numerical results for the prototypical water/1,2-dichloroethane system. These results show that the parallel components of the dielectric permittivity tensor can be accurately extracted. In contrast, the perpendicular component does not converge to the correct bulk value at large distances from the LLI, highlighting a flaw in the regularly applied coarse-graining procedure.     

基于风洞的设备健康管理与数据有效性判定平台研究

低速增压风洞是满足我国航空工业科技发展而建设的一座气动力重大基础试验设施。为了保障该设施的高效率和可靠地运行,以各机电设备、电气测控设备、机械装置为对象,根据其故障模式和故障特点选取合适的监测点,获取实时工作状态数据,再以数据为基础,进行状态监测、故障诊断、故障预测,实现预先性决策和针对性快速维修。基于OSA-CBM 体系构建的风洞健康管理系统,根据设备的运行状态,实现对试验数据的有效性进行实时判定,并实现了风洞装备由事后维修向视情维修转变;实现了装备从使用、维护、管理模式由分散式管理向集约式管理的转变;实现了装备系统故障诊、预测及判读从人工智能向机器智能的转变。     

多速率STFT超宽带信号瞬时频率估计研究

提出多速率短时傅里叶变换(Multi Rate Short Time Fourier Transform,MR-STFT)瞬时频率估计算法,提高了超宽带信号瞬时频率估计精度。该方法将多速率信号处理算法与短时傅里叶变换(STFT)技术相结合,兼顾采样频率和被测频率,将宽频范围进行分段采样,对分段处理结果进行拟合,构成多速率STFT算法,实现超宽带信号瞬时频率的高精度测量。论文通过对仿真信号和实测信号进行处理,研究了方法的可行性和频率估计精度,结果表明MR-STFT算法较大提高了超宽带信号瞬时频率估计精度,尤其对低信噪比的超宽带信号效果显著。     

Progress in wind tunnel experimental techniques for wind turbine

Based on the unsteady aerodynamics experiment (UAE) phase VI and the model experiment in controlled conditions (MEXICO) projects and the related research carried out in China Aerodynamic Research and Development Center (CARDC), the recent progress in the wind tunnel experimental techniques for the wind turbine is summarized. Measurement techniques commonly used for different types of wind tunnel experiments for wind turbine are reviewed. Important research achievements are discussed, such as the wind tunnel disturbance, the equivalence of the airfoil inflow condition, the three-dimensional (3D) effect, the dynamic inflow influence, the flow field structure, and the vortex induction. The corresponding research at CARDC and some ideas on the large wind turbine are also introduced.     

分裂导线自阻尼振动特性研究

为了掌握线路的振动状态,确定线路抗振能力,保证线路安全,需要明确架空输电导线的风致振动响应．本文针对江苏境内某特高压工程LGJ-630/45型导线,建立其振动控制能量平衡方程,编制了Fortran程序以高效准确地求解该超越方程,计算分析了单导线及四种分裂导线微风振动状态下的振动及耗能特性．结果表明,单导线在风振平衡点处的双振幅最大值在最低频率上,约为导线直径的两倍;四种分裂导线风振平衡点处的幅值在15Hz附近达到最大值;导线单位长度功耗在60Hz附近达到最高,功耗能力在较低频域(10Hz~20Hz)上较弱,在较高频域(30Hz~80Hz)较强;导线分裂数越大,分裂导线的振幅越小,八分裂导线的防振消振效果相对最好;四种分裂导线在在10Hz~20Hz频域振动幅值大而单位功耗水平低,因此10Hz~20Hz频段是分裂导线的危险频段,防振措施应该针对这一频段设置．研究方法与成果为LGJ-630/45导线的抗振设计提供了科学依据．