汽轮机叶片间流体流动的模拟研究

对超音速汽轮机的叶片间可压缩流体的流动情况进行了模拟研究。在对Giel等人的实验研究结果进行分析的基础上,将转子设计为流向转角为136°和轴向弦长为12.7 cm。通过Fluent软件对各种模型在湍流条件下反射边界情况(RBC)及非反射边界情况(NRBC)进行了二维数值模拟。研究结果对超音速汽轮机的优化设计提供了参考。     

大气湍流中光传播的数值模拟

大气分子等粒子的存在对光的空间传播通常会产生光束的扩展、漂移等的影响.文中在随机媒质中光的传播理论的基础上,分析了构造大气湍流随机相位屏所需要的条件,采用McGlamery算法和Huygens-Fresnel原理,数值模拟给出了Kolmogorov谱下的大气湍流随机相位屏.分析了光波从发射机经湍流大气传播到达接收机平面时的光场变化特征.模拟分析表明:大气分子等粒子的存在,对光的振幅及能量的空间分布均造成很大的影响.     

壁湍流周期性吹吸减阻的实验研究

为了研究局部周期性吹吸小扰动对湍流边界层的影响和湍流相干结构减阻控制机理,用实验方法研究了局部周期性吹吸小扰动与湍流边界层的相互作用.采用热线测速技术精细测量了施加吹扰动前后平板湍流边界层不同法向位置的流向、法向和展向速度分量的时间序列信号;通过测量扰动源下游近壁区域平均速度剖面的变化,发现在扰动下游一定空间范围内,粘性底层增厚和壁面减阻;通过对湍流度变化的分析,发现扰动影响猝发的发生;此外通过对展向平均涡量变化的分析发现,在扰动下游形成了2个定常的、强度相似的、大尺度的展向涡,它们起到流体滚动轴承的作用,减小了壁面摩擦阻力.     

Numerical study on the restriction speed of train passing curved rail in cross wind

The results of numerical investigations of aerodynamic forces and moment coefficients of flow passing a simplified train geometry under different wind speeds are summarized. To compute numerically the different coefficients, the three-dimensional Reynolds-Averaged Navier-Stokes (RANS) equations, combined with the k-ε turbulence model, were solved using finite volume technique. The pres-sure-velocity fields were coupled using the SIMPLE algorithm. At each iteration the pressure correction was obtained by sol...     

基于湍流自旋理论的二维方腔旋转流动的数值模拟

基于湍流自旋理论对旋转方腔内不可压流体的流动进行了二维数值模拟,用有限容积法在交叉网格上对控制方程进行离散,采用SIMPLEC算法进行计算,对流项的离散方面采用了延迟修正的QUICK格式,最后采用二维的TDMA算法进行迭代求解,并对边界条件处理采用了Block块技术.同时与经典理论即Navier-Stokes（N-S）方程的模拟情况做了比较.得出下列结论：N-S方程表明方腔旋转时内部流体只会作刚体旋转;而自旋模型表明该类流动具有不平凡性和不稳定性：即流体的内聚力不足以使流体跟随固体边界作刚体运动,旋转边界必然在流体中诱导出小尺度耗散涡旋,这些小尺度涡旋在固壁附近组织出正负相间的拓扑缺陷（涡旋场强）,这一流体定向奇性会与速度场耦合,并容易形成复杂的大尺度的涡旋运动.     

The use of a mixing-sensitive chemical reaction for the study of pulp fibre suspension mixing

The competitive, consecutive chemical reactions between 1-naphthol and diazotized sulfanilic acid were utilized to study the mixing of a pulp fibre suspension in a 22 L stirred tank reactor. Mixing quality was determined from the distribution between the mono and bis substituted reaction products once a correlation was made for the adsorption of the product dyes onto the suspended fibres. The technique was found to be adequate for assessing micromixing and turbulence intensity within a fibre suspension provided the measured product distribution, Xs, was between 0.4 and 0.01. Thus the mixing conditions that could be assessed depended on both the energy dissipation within the mixer and the amount of the fibre present. For the experimental conditions chosen for this study energy dissipation rates would typically have to be less than 80 W/kg and the suspension mass concentration less than 2.5%. When compared with water, a reduction in turbulence levels at both the impeller zone and a remote zone in the stirred vessel was observed for fibre mass concentrations as low as 0.5%. The turbulence decreased as the suspension mass concentration was increased. This decrease is attributed to energy dissipation by friction at fibre-fibre contact points as the fibres move relative to one another in the flow. This sink removes energy from the turbulence cascade which never shows up as small-scale fluid deformations leading to better mixing.     

典型超高层建筑横风向气动力谱的构成分析

通过风洞试验得到典型超高层建筑的横风向脉动风荷载分布,将横风向脉动风荷载作用分解为横向紊流及旋涡脱落2种作用机理的共同作用,分析了横风向气动力谱的构成成分,并将分析结果与高频动态测力天平的结果进行了对比研究．结果表明:横向紊流对横风向气动力谱的贡献较小,而旋涡脱落激励对总横风向气动力谱的贡献较大;在不同风场中这些贡献量会发生改变．根据同步测压试验分解横风向气动力谱的方法可以清楚地解释超高层建筑横风向气动力谱的构成成分．     

Predicting airflow distribution and contaminant transport in aircraft cabins with a simplified gasper model

This study investigated the air distribution and contaminant transport in aircraft cabins with gaspers by using computational fluid dynamics (CFD). If the detailed gasper geometry were used in the CFD simulations, the grid number would be unacceptably high. To reduce the grid number, this investigation proposed a method for simplifying the gasper geometry. The method was then validated by two sets of experimental data obtained from a cabin mockup and a real aircraft cabin. It was found that for the cabin mockup, the CFD simulation with the simplified gasper model reduced the grid number from 1.58 to 0.3 million and the computing cost from 2 days to 1 hour without compromising the accuracy. In the five-row economy-class cabin of the MD-82 airplane, the CFD simulation with the simplified gasper model was acceptable in predicting the distribution of air velocity, air temperature, and contaminant concentration.     

Inflow turbulence generation techniques for large eddy simulation of flow and dispersion around a model building in a turbulent atmospheric boundary layer

The present paper investigates the performance of various inflow turbulence generation techniques (ITGT) for large eddy simulation (LES) of flow and dispersion around a model building in a turbulent atmospheric boundary layer. Four different ITGT comprising 1 – no fluctuations, 2 – spectral method, 3 – vortex method and 4 – internal mapping, based on two basic methodologies (i.e. precursor and synthetic turbulence methods), are employed. These techniques are evaluated by considering their prediction accuracy, computational costs, complexity of implementation, inflow information required to operate and impacts on the flow downstream of the inlet, particularly in the wake region of the model building. Results indicate that the accuracy of LES predictions is greatly reliant on ITGT. It is shown that ITGT not only have significant effects on flow field vortical structures, but also influence frequency contents of velocity fluctuations, recirculation regions and plume shapes in the wake region.     

附加湍流器强化油田采出水超滤过程的研究

为改善超滤处理油田采出水的膜过滤性能，设计了4种不同结构形式的湍流器并进行膜过滤强化试验，考察了湍流器的构型、螺距等对膜通量及单位产水能耗的影响。结果表明，湍流器可以明显提高膜通量，同时降低了单位产水能耗。与未加湍流器的相比，在相同的操作条件下采用湍流器可以使膜渗透通量提高83％～164％，而单位产水能耗却降低了31％～42％，其中螺距为20．0mm、缠绕线粗为1．0mm缠绕式湍流器的实际使用效果最为显著。