一种修正的低温流体空化流动计算模型

为了更准确地预测低温流体的空化流动特性, 基于Kubota空化模型, 对蒸发和凝结源项进行修正, 建立了一种考虑热力学效应的空化模型. 分别采用原始和修正的Kubota空化模型, 计算了绕对称回转体液氮的空化流动, 通过与实验结果的比较对修正的空化模型进行了评价. 结果表明, 与原Kubota空化模型比较, 修正的空化模型由于考虑了热力学效应, 计算获得的蒸发量减小, 凝结量增大, 空穴长度减小, 空穴界面形态呈模糊状态.计算结果与实验结果更加一致, 说明修正的空化模型能准确的描述低温流体空化过程的质量传输过程, 能够更准确模拟低温流体中的空化流动特性.      

低温介质质量传输空化模型的代理分析及优化

利用基于代理模型的整体敏感度分析方法,对考虑模型参数和物质属性的低温介质质量传输空化模型进行了评价,从而获得影响预测精确度的主要因素,并对空化模型参数进行了校准。结果表明：凝结系数对压力和温度预测精度的影响较大,整体敏感度分别为44%和29%;蒸发系数的影响较小,整体敏感度均小于5%。通过代理模型优化分析获得了Merkle空化模型对压力和温度的预测精度随凝结系数的变化趋势：当凝结系数小于20时,随凝结系数的增大,压力预测精度提高,温度预测精度降低;当凝结系数大于20时,压力和温度的预测精度均随凝结系数的增大而降低。优化后的蒸发系数和凝结系数分别为3.8和19.43,满足Pareto最优解,模型预测能力得到提高。     

PANS模型在空化湍流数值计算中的应用

采用一种基于标准k-ε模型改进的局部时均化模型（Partially-Averaged Navier-Stokes Model,PANS）,并应用于空化流动计算。控制不同的模型参数,分别对绕平头轴对称回转体和Clark-Y型水翼的空化流动进行模拟,并与实验结果进行对比。结果表明：PANS模型中未分解湍动能比率fk的取值对预测空化流动的数值计算精度有重要影响,改变fk的取值可实现对不同滤波尺度范围内的求解;随着fk值的减小PANS的预测精度逐步提高,能在相对较大范围内求解较小尺度的湍流运动过程中,预测到湍流运动中强烈的非定常特性;同时可以比较准确地预测空化流场结构和动力特性。     

考虑当地涡旋运动修正的湍流模型在非定常空化湍流流场计算中的应用

为了更精确地模拟当地涡旋运动对复杂非定常空化湍流流动的影响,考虑当地涡旋运动特性对标准k-ε湍流模型进行了修正;并采用该修正模型对二维Clark-Y水翼周围非定常空化湍流场进行了计算;通过与实验结果进行对比,分析并验证了该修正模型计算结果的有效性。研究表明:该修正湍流模型根据当地涡旋效应对湍动能输运方程中的生成项进行修正,可以有效解决标准k-ε模型对湍动能的过度预测问题,得到的空化核心区域时均湍动能和湍流黏性的预测结果降低了约30%,与实际值更为接近;标准k-ε模型计算所得的时均空泡长度不大于0.6倍弦长,而修正模型计算所得的时均空穴可以覆盖水翼吸力面;修正模型可以准确预测水翼吸力面表面空泡的非定常脱落过程,包括附着空穴的拉伸和断裂,以及脱落空泡的逐渐消失。     

液氮过冷流动沸腾数值模拟中的双流体模型

液氮过冷流动沸腾广泛见于各种低温换热设备中.采用双流体模型分析液氮过冷流动沸腾,需要为模型提供适当的封闭方程,用于描述汽液两相间质量、动量以及能量的传输过程,封闭方程的合理性直接决定了双流体模型的准确性.将液氮流动沸腾通道划分为近壁区和主流区,分别介绍液氮核态沸腾壁面上的传热传质机理模型,以及两相流程内汽液之间的相互作用的相间传输模型,建立液氮流动沸腾过程适用的双流体模型,并分析了对模型预测能力具有显著影响的因素,指出存在的问题和解决方案.      

土体水分传输的温度效应试验系统设计与应用

自制了一套用于研究温度作用下土体水分传输机制的室内试验模拟系统.采用水浴加热替代电阻丝直接加热的方案,解决加热不均匀且不容易控制温度的难题.应用串行通讯接口技术把智能温度控制仪表和微机连接,实现了温度自动控制和采集的自动化.开展了7组试验耗时接近1年,试验结果表明,该系统性能稳定、部件之间兼容性较好,连续工作30天温度...     

考虑方向效应的钢纤维混凝土损伤破坏数值分析

钢纤维的平均方向效应系数是表征纤维综合取向性对混凝土性能影响的一个重要因素。为了从细观层次探究平均方向效应系数对钢纤维增强混凝土复合材料损伤开裂的影响,本研究基于有限元软件参数化语言,建立了由钢纤维、水泥砂浆以及界面过渡区三相材料构成的二维钢纤维混凝土模型,并模拟了不同平均方向效应系数下钢纤维混凝土单轴拉伸破坏的全过程。结果表明：混凝土的抗拉强度随着平均方向效应系数的增大而提高;钢纤维对混凝土的阻裂增韧效应也随之增强,进一步揭示了钢纤维混凝土在单轴拉伸条件下混凝土的损伤破坏机理。     

考虑气核生长溃灭效应的螺旋桨梢涡空化初生数值模拟研究

梢涡空化是螺旋桨最早发生的空化类型,其一旦发生会显著增强舰船辐射噪声水平.因此,螺旋桨梢涡空化初生的预报是军舰临界航速确定的关键,长期以来受到船舶领域诸多专家学者的重点关注.微观气核受涡心低压作用而发生暴发式生长是梢涡空化初生的重要机制,而传统欧拉框架下的宏观空化模型用经验参数模化了微观气核的影响而无法对该过程准确模拟,影响对螺旋桨空化初生的准确预报.为了弥补传统模拟方法的不足,本研究发展并使用一种基于气泡动力学并考虑水相可压缩效应的欧拉-拉格朗日空化初生数值预报方法对螺旋桨梢涡空化初生进行了数值模拟研究.与实验结果对比表明,该模型能够准确地预报螺旋桨梢涡空化初生.此外,本研究不仅从微观气核角度探究不同来流气核尺寸对空化初生的影响,还进一步研究梢涡流动特性对气核演变的影响机制,初步探究初生空化在螺旋桨梢涡流场中的发声机理.在空化初生光学判断准则下尺寸越大的气核越容易被梢涡捕获而暴发式生长.气核在梢涡卷吸作用下逐渐靠近涡心低压区.在涡心低压区的持续作用下气核开始暴发式生长,并在半径达到最大后迅速收缩溃灭,产生强烈的正声压脉冲信号.     

纳米粒子在方管中传输与沉降的研究

采用有限体积法离散并应用Simple方法对方截面弯曲管道内的纳米粒子传输和沉降进行了数值计算,结果表明Reynolds数和Schmidt数是影响纳米粒子传输和沉降的重要参数。粒子较小时,弯管中轴向速度较大的区域就是粒子的高浓度区域,沉降增强因子最大值出现在外弯侧的中心位置;粒子较大时,截面浓度的梯度值降低,沉降增强因子趋于平均,此时整个截面的粒子平均沉降。弯曲作用对于粒子较大且Dean数也较大时的影响更加明显。     

改进WENO格式及其在爆轰计算中的应用

对已有的一种改进型WENO-M格式进行了理论上的修正,得到了新的WENO权函数。与原WENO-M格式相比,新得到的WENO-M-P格式减少了约9%的CPU计算时间,同时也保证了在一阶极值点处不降低精度（经典的WENO格式在一阶极值点处精度下降）,仍然保持5阶精度。为了验证修正后的格式,采用二步反应模型数值模拟了几组一维和二维爆轰：在一维爆轰模拟中,对比了WENO-M格式和WENO-M-P格式在一定温度下的最低起爆压强以及一定压强下的最低起爆温度;在二维旋转爆轰的模拟中,对比了WENO-M格式和WENO-M-P格式的计算效果。结果表明：在同样的起爆温度下,WENO-M 格式和 WENO-M-P 格式的最低起爆压强均高于 WENO格式,但WENO-M-P格式比WENO-M格式的最低起爆压强低;三种格式在不同压强下的最低起爆温度相同;WENO-M-P格式具有和WENO-M格式一样的计算效果,优势是节省了计算时间。     

Numerical simulation of gap effect in supersonic flows

The gap effect is a key factor in the design of the heat sealing in supersonic vehicles subjected to an aerodynamic heat load. Built on S-A turbulence model and Roe discrete format, the aerodynamic environment around a gap on the surface of a supersonic aircraft was simulated by the finite volume method. As the presented results indicate, the gap effect depends not only on the attack angle, but also on the Mach number.     

Time‐dependent turbulent cavitating flow computations with interfacial transport and filter‐based models

Turbulent cavitating flow computations need to address both cavitation and turbulence modelling issues. A recently developed interfacial dynamics‐based cavitation model (IDCM) incorporates the interfacial transport into the computational modelling of cavitation dynamics. For time‐dependent flows, it is known that the engineering turbulence closure such as the original k–ε model often over‐predicts the eddy viscosity values reducing the unsteadiness. A recently proposed filter‐based modification has shown that it can effectively modulate the eddy viscosity, rendering better simulation capabilities for time‐dependent flow computations in term of the unsteady characteristics. In the present study, the IDCM along with the filter‐based k–ε turbulence model is adopted to simulate 2‐D cavitating flows over the Clark‐Y airfoil. The chord Reynolds number is Re=7.0 × 10⁵. Two angles‐of‐attack of 5 and 8° associated with several cavitation numbers covering different flow regimes are conducted. The simulation results are assessed with the experimental data including lift, drag and velocity profiles. The interplay between cavitation and turbulence models reveals substantial differences in time‐dependent flow results even though the time‐averaged characteristics are similar. Copyright © 2005 John Wiley & Sons, Ltd.     

水流冲击管道内滞留气团现象的VOF模型仿真分析

针对复杂管道系统内水流冲击滞留气团现象,采用VOF模型(Volume of Fluid Model)进行了数值模拟计算,并与一维模型进行了比较计算分析,结果表明:系统的最大压力并不总是气团的最大压力,有可能还会叠加水体对管壁的撞击而形成的突然升高压力.与实验实测结果的比较分析表明:采用VOF模型,能够较精细地仿真水流冲击滞留气团现象的气团形态、流场结构以及压力分布等的变化过程,其压力数值计算结果与实验实测基本吻合,其计算误差明显小于现有一维模型的计算误差,是深入研究该复杂瞬变流现象的有效方法.     

Implementation of phase change thermodynamic probability for unsteady simulation of cavitating flows

The aim of this work is to investigate the non‐equilibrium effects of phase change in cavitating flows. For this purpose, the concept of phase change thermodynamic probability is used along with homogeneous model to simulate two‐phase cavitating flows. For simulation of unsteady behaviors of cavitation, which have practical applications, unsteady PISO algorithm based on the non‐conservative approach is utilized. For multi‐phase simulation, single‐fluid Navier–Stokes equations, along with the volume fraction transport equation, are employed. In this paper, phase change thermodynamics probabilities and cavitation model is briefly summarized. Thus, derivation of the cavitation model, starting from the basic thermodynamic equations to the mass and momentum conservation equations at a liquid–vapor two‐phase flow, is presented to explain the numerical model. Unsteady simulations of cavitation around a flat plate normal to flow direction are presented to clarify the accuracy of the model. The accuracy of the numerical results is good, and it is possible to apply this method to more complex geometries. Copyright © 2010 John Wiley & Sons, Ltd.     

Electromagnetohydrodynamic flows and mass transport in curved rectangular microchannels

Curved microchannels are often encountered in lab-on-chip systems because the effective axial channel lengths of such channels are often larger than those of straight microchannels for a given per unit chip length. In this paper, the effective diffusivity of a neutral solute in an oscillating electromagnetohydrodynamic(EMHD)flow through a curved rectangular microchannel is investigated theoretically. The flow is assumed as a creeping flow due to the extremely low Reynolds number in such microflo...     

Finite element analysis of multicomponent two-phase flows with interphase mass and momentum transport

The application of the finite element method to multiphase flow problems with interphase mass and heat transfer is described. A general forinulation is used that determines the position of the interfacial boundary and allows for multiple solvents, differential volatilities and concentration- and temperature-dependent thermophysical properties. Species phase change and the dramatic volume change that acompanies interphase mass transfer make implementation of the theory challening, since these events lead to discontinuous velocities and concentrations at phase boundaries. These discontinuities are especially large in processes involving rapid evaporation or condensation. As examples we examine the effects of rapid drying on film and fibre formation of sol--gel materials, which are often laden with volatile species.     

Multiscale computations of thin films in multiphase flows

In multiphase flows thin films are often encountered when fluid masses collide. These films can become very thin and in direct numerical simulations (DNS) it is often impractical to resolve their thickness fully, even with adaptive grid refining. Here we examine the collision of a fluid drop with a wall and develop a multiscale approach to compute the flow in the film between the drop and the wall. By using a semi-analytical model for the flow in the film we capture the evolution of films thinner than the grid spacing reasonably well.     

Study on the thermal protection performance of superalloy honeycomb panels in high-speed thermal shock environments

The thermal protection performance of superalloy honeycomb structure in high-temperature environments are important for thermal protection design of high-speed aircrafts. By using a self-developed transient aerodynamic thermal simulation system, the thermal protection performance of superalloy honeycomb panel was tested in this paper at different transient heating rates ranging from 5°C/s to 30°C/s, with the maximum instantaneous temperature reaching 950°C. Furthermore, the thermal protection performance of superalloy honeycomb structure under simulated thermal environments was computed for different high heating rates by using 3D finite element method, and a comparison between calculational and experimental results was carried out. The results of this research provide an important reference for the design of thermal protection systems comprising superalloy honeycomb panel.     

翼型空泡周期性流动的数值模拟及机理分析

采用基于正压关系的均质平衡流空化模型和低雷诺数修正的k-ε湍流模式,自行开发了空泡流数值模拟方法和计算软件,对绕翼型空泡的周期性流动现象进行了数值模拟.计算结果与实验数据的对比表明,空泡的宏观特征、流动特性、周期性脱落的斯坦顿数St等与试验结果接近,验证了计算结果的可靠性.空泡在大约一个周期的2/3时间段内成长,并在大约1/3周期时刻发生断裂脱落.这两个特征时间与高速摄像实验结果一致.所取工况对应的组合参数σ/2α=2.865,以翼弦长计算可得St=0.217,与文献的最新试验结果吻合.空泡周期性运动过程中升阻系数也周期性振荡,时均值C<,1>=0.41,C<,d>=0.097,振荡频率与空泡脱落频率一致.对空泡运动过程中流场结构的变化进行了分析,结果表明在大攻角条件下,空泡闭合区后的逆压梯度导致涡的形成及回射流的发展,沿壁面逆向流动的混合介质射流是引起空泡断裂的原因,回射流发展、涡结构变化与空泡非稳态演化过程存在密切的联系,探讨了翼型空泡发生周期性脱落的一些机理.