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1.
采用格子Boltzmann方法(LBM)和改进的插值格子Boltzmann方法(GILBM)研究了45°斜方腔的顶盖驱动流和Roach通道内的流动特性,并与基准解进行了对比。结果表明,对于45°斜方腔的顶盖驱动流,当雷诺数较小时,两种方法的计算结果与基准解吻合较好;但当雷诺数较大时,采用LBM的计算结果准确性降低,而基于GILBM方法得到的结果准确度升高,且计算稳定性好。对于Roach通道内的流体流动而言,两种方法的计算精度和复杂边界的复杂程度与雷诺数大小有关。根据流场边界形状的复杂程度,网格划分与计算精确度的不同要求,两种方法各有利弊。  相似文献   

2.
并列圆柱绕流的格子Boltzmann数值模拟   总被引:1,自引:0,他引:1  
采用非均匀不可压格子Boltzmann模型对低雷诺数下并列圆柱绕流进行了数值模拟,给出了数值计算结果,分析了间距g对圆柱尾流及升力、阻力的影响,并在此基础上得到了4种尾迹模式.此外,研究了流场的初始扰动对流动分岔现象的影响,发现在适当的扰动下可以很快得到同步同相的尾流.对Re=160和200下圆柱的升、阻力进行了对比,结果表明升力和阻力受间距g的影响大于雷诺数.  相似文献   

3.
流向振荡圆柱绕流的格子Boltzmann方法模拟   总被引:1,自引:0,他引:1  
龚帅  郭照立 《力学学报》2011,43(1):11-17
用一种新近发展起来的格子Boltzmann方法(LBM)在相对较小的雷诺数(Re≤200)条件下模拟了不可压缩的流向振荡圆柱绕流问题,考查了涡脱落模态和升阻力特性.通过模拟,在近尾流区发现了实验研究中已经发现的对称/反对称的涡脱落模态,包括有些传统数值方法未发现的模态.研究了频率锁定区域的范围及其与振幅的关系,发现振幅越大,发生锁定的频率区域越宽.此外还对升阻力进行了定量意义的模拟,研究了振荡频率和振幅与升阻力的关系.  相似文献   

4.
为了研究三维串联多圆柱绕流在不同圆柱间距比L/D(L为圆柱的间距,D为圆柱直径)情况下的尾涡结构,基于格子玻尔兹曼(LBM)方法,采用大涡模拟(LES)方法计算了高雷诺数下三维单圆柱及三维串联多圆柱在不同L/D情况下的尾涡流场。数值结果表明:LBM-LES方法可以较好地模拟出三维单圆柱以及串联多圆柱的尾涡结构;高雷诺数下单圆柱绕流尾迹变化具有不稳定性;串联多圆柱绕流存在临界间距比L/D=4,当圆柱间距比小于临界间距比时,圆柱间不会产生尾涡脱落;当圆柱间距比大于临界间距比时才会产生明显的涡脱落现象,且前方圆柱脱落的涡对后方圆柱有冲击作用,会对后方圆柱的升/阻力系数振动幅值有一定的影响;串联多圆柱绕流的上下游时均阻力系数曲线在临界间距比时会发生转折,呈逐渐增大趋势;当圆柱间距比小于临界间距比时,在下游圆柱前增加圆柱会对下游圆柱以及中游圆柱的时均阻力系数产生影响,而当圆柱间距比大于临界间距比时,在下游圆柱前增加圆柱对下游圆柱以及中游圆柱的时均阻力系数基本没有影响。  相似文献   

5.
横向振荡圆柱绕流的格子Boltzmann方法模拟   总被引:1,自引:0,他引:1  
龚帅  郭照立 《力学学报》2011,43(5):809-818
基于格子Boltzmann方法(LBM)对不可压横向振荡圆柱绕流问题进行了数值研究. 与传统的求解宏观的N-S方程的数值方法不同, LBM求解此类问题不需要采用动网格, 而且不需要对网格进行特殊处理, 从而节约了计算成本. 结果显示, 当振荡频率增加到相应的静止圆柱绕流的自然涡脱落频率附近时, 圆柱后最新形成的集中涡距离柱体越来越近, 直到达到一个极限位置. 随后, 集中涡突然转向圆柱体另一侧脱落. 当振荡频率接近于静止圆柱的自然涡脱落频率时, 发生频率同步的现象. 随着振荡频率远离自然涡脱落频率, 同步现象消失. 在几种次谐振荡和超谐振荡下, 尾流区的涡脱落频率仍为相应的静止圆柱绕流的自然涡脱落频率.  相似文献   

6.
利用有限体积法实现了基于非正交同位网格的SIMPLE算法。基于熵分析方法,采用涡粘性模型求解湍流熵产方程,系统研究了湍流模型对二维翼型绕流流场熵产率的影响。通过计算NACA0012翼型在来流雷诺数为2.88×106时,0°攻角~16.5°攻角范围内的翼型表面压力系数分布和升阻力特性,验证了算法及程序的正确性。结果表明,选择不同湍流模型时,翼型流场熵产的计算结果存在差异,湍流耗散是引起流场熵产的主要原因;翼型流场的熵产主要发生在翼型前缘区、壁面边界层和翼型尾流区域,流场熵产率与翼型阻力系数线性相关;当产生分离涡时,粘性耗散引起的熵产下降。  相似文献   

7.
通过结合格子Boltzmann方法(LBM)和DF(Direct Forcing)/FD(Fictitious Domain)思想,建立了一种新的LB-DF/FD方法。采用两套网格系统,欧拉网格用于流体,拉格朗日网格用于固体,有效地避免了计算中重新生成网格的步骤,同时在处理流固问题方面优于LBM方法。通过模拟通道中单圆柱旋转的流场,验证了该方法的正确性;并利用该方法模拟了低雷诺数下通道中并列旋转圆柱周围的流场,分析了圆柱距离壁面间距gw和雷诺数Re对流场结构的影响。研究结果表明:gw显著影响了流场的结构及圆柱的受力;而Re对圆柱升力及Stokes单元数目的影响较大。  相似文献   

8.
利用有限体积法实现了基于非正交同位网格的SIMPLE算法。基于熵分析方法,采用涡粘性模型求解湍流熵产方程,系统研究了湍流模型对二维翼型绕流流场熵产率的影响。通过计算NACA0012翼型在来流雷诺数为2.88×106时,0°攻角~16.5°攻角范围内的翼型表面压力系数分布和升阻力特性,验证了算法及程序的正确性。结果表明,选择不同湍流模型时,翼型流场熵产的计算结果存在差异,湍流耗散是引起流场熵产的主要原因;翼型流场的熵产主要发生在翼型前缘区、壁面边界层和翼型尾流区域,流场熵产率与翼型阻力系数线性相关;当产生分离涡时,粘性耗散引起的熵产下降。  相似文献   

9.
基于LBM的壁湍流跨尺度能量传递结构统计   总被引:1,自引:1,他引:0  
高铨  邱翔  夏玉显  李家骅  刘宇陆 《力学学报》2021,53(5):1257-1267
壁湍流不同尺度间能量传输特性存在着明显的各向异性, 了解能量不同尺度间传递的空间分布是进一步构造高保真各向异性大涡模拟亚格子模式的前提. 基于格子Boltzmann数值(lattice Boltzmann method, LBM)模拟方法对雷诺数$Re_{\tau } =180$的槽道湍流进行直接数值模拟. 结果与公开的槽道湍流数据库进行对比, 平均速度剖面、雷诺应力和脉动速度均方根均取得了较好的一致性, 验证了LBM方法模拟槽道湍流的可靠性. 对模拟后的数据采用空间滤波方法得到不同尺度间能量交换量的空间分布场, 结合结构识别捕捉方法——聚类分析法对不同尺度间能量传输结构的空间分布特性进行了分析. 结果表明尺度间能量传输结构在全流场物理空间中主要为小尺寸结构, 结构的体积概率密度呈现出$-$4/5幂律, 按结构距壁面最小距离以结构距壁面距离又可将结构划分为附着结构和分离结构, 其中附着结构以较小的数量占比达到了较高的体积占比, 表明附着结构多为大尺寸结构, 进一步的对附着结构的统计表明结构在尺寸上存在着一定的幂律关系, 表明不同尺度间能量输运结构也具有Townsend提出的附面涡的自相似性, 最后对能量正反传附着结构的成对特性研究发现, 能量正传$\!-\!$反传结构对倾向于沿展向并排排列.   相似文献   

10.
本文给出了关于亚临界雷诺数二维圆柱绕流动态特性的实验结果。应用热膜、热线和压力传感器测量了壁面剪切应力脉动、壁面压力脉动和流场的速度脉动,给出了壁面剪切应力脉动频率在驻点附近和分离前后变化的特征,计算了这些脉动量在圆柱面上任意两点间的相关特性。实验结果表明,在亚临界雷诺数二维圆柱绕流的边界层流场中存在着一个频率与涡脱落频率相同的整体同步脉动。  相似文献   

11.
The effects of two parallel porous walls are investigated, consisting of the Darcy number and the porosity of a porous medium, on the behavior of turbulent shear flows as well as skin-friction drag. The turbulent channel flow with a porous surface is directly simulated by the lattice Boltzmann method (LBM). The Darcy-Brinkman- Forcheimer (DBF) acting force term is added in the lattice Boltzmann equation to simu- late the turbulent flow bounded by porous walls. It is found that there are two opposite trends (enhancement or reduction) for the porous medium to modify the intensities of the velocity fluctuations and the Reynolds stresses in the near wall region. The parametric study shows that flow modification depends on the Darcy number and the porosity of the porous medium. The results show that, with respect to the conventional impermeable wall, the degree of turbulence modification does not depend on any simple set of param- eters obviously. Moreover, the drag in porous wall-bounded turbulent flow decreases if the Darcy number is smaller than the order of O(10-4) and the porosity of porous walls is up to 0.4.  相似文献   

12.
A wall‐driven incompressible viscous flow in a ½ circular cavity is simulated, based on the lattice Boltzmann method (LBM). The treatment of curved boundary with second‐order accuracy is used. The force evaluation is based on the momentum‐exchange method. The streamlines and vorticity contours and the velocity component along the central line of a semi‐circular cavity are obtained for different Reynolds numbers. The numerical results show that the LBM can capture the formation of primary, secondary and tertiary vortices exactly as the Reynolds number increases and has a great agreement with those of current literatures. Copyright © 2008 John Wiley & Sons, Ltd.  相似文献   

13.
基于插值补充格子波尔兹曼方法和幂律流体的本构方程,建立了贴体坐标系下适用于幂律流体的格子波尔兹曼模型,模拟了幂律流体的圆柱绕流问题,采用非平衡外推格式处理圆柱表面的速度无滑移边界,利用应力积分法确定曳力系数和升力系数,并与基于标准的格子波尔兹曼方法和有限容积法获得的数值数据进行对比,吻合良好. 进行了网格无关性验证之后,分析了稳态流动时,不同雷诺数下幂律指数对于尾迹长度、分离角、圆柱表面黏度分布、表面压力系数及曳力系数的影响,以及非定常流动中,幂律指数对于流场、曳力系数、升力系数和斯特劳哈尔数的影响. 获得的变化规律与基于其他数值模拟方法得到的结果相一致,充分验证了模型的有效性和正确性. 结果表明:插值补充格子波尔兹曼方法可以用来模拟幂律流体在具有复杂边界流场内的流动问题,通过引入不同的非牛顿流体本构方程,该方法还可以进一步应用于其他类型的非牛顿流体研究中.  相似文献   

14.
In the lattice Boltzmann method (LBM), the mechanism of fluid–solid interaction can be effectively captured by appropriately enforcing the no‐slip conditions in shear direction, and bounce‐back of the non‐equilibrium distribution portion in the normal direction at fluid–solid interfaces. Among various solid–fluid interaction schemes being proposed for LBM in recent decades, two simple fluid–solid interaction methods—the momentum exchange algorithm (MEA) and the immersed boundary scheme (IBS)—were developed based on the above concept. In this paper, MEA and IBS are implemented in a D2Q9 LBGK system and applied to measure the wall correction factors of drag force upon a stationary circular particle midway in the Poiseuille channel flow at very low Reynolds number and drag coefficients at low to moderate Reynolds numbers. MEA and IBS are also employed to compare the fluid‐induced torque over the cylinder in the Taylor–Couette flow, and the steady velocity of a particle settling under the influence of gravity inside a tube. The above experiments show that IBS seems to be more accurate and less demanding on lattice resolution. Copyright © 2010 John Wiley & Sons, Ltd.  相似文献   

15.
This paper deals with the investigation of flow field due to clap and fling mechanism using immersed boundary coupled with lattice Boltzmann method. The lattice Boltzmann method (LBM), an alternative to Navier–Stokes solver, is used because of its simplicity and computational efficiency in solving complex moving boundary problems. Benchmark problems are simulated to validate the code, which is then used for simulating flow over two elliptic wing of aspect ratio 5 performing clap and fling flapping motion for different flow parameters such as Reynolds number (Re=75, 100, 150), advance ratio (J=10E−3.10E−2,0.2) and frequency (f=0.05 Hz, 0.25 Hz). Numerical simulation is able to capture typical low Reynolds number unsteady phenomena such as, ׳wake vortex wing interaction׳, ׳Kramer effect׳ and ׳delayed stall׳. The results are both qualitatively and quantitatively consistent with experimental observation. The parametric study involving different combinations of Re, f and J depict distinctly different aerodynamic performances providing physical insights into the flow physics. It is observed that a combination of low f, low J and high Re flow results in better aerodynamic performance. Pronounced lift enhancement via leading edge vortices are obtained in unsteady regime (J<1) compared to quasi-steady regime (J>1). The role of leading edge vortices in enhancing lift are investigated by studying the size and strength of these vortices for different flow conditions. For a given Re, the magnitude of maximum lift coefficient decreases with increasing f irrespective of the value of J; while the same is enhanced with the increasing Re.  相似文献   

16.
对于Oldroyd-B型黏弹性流体,本文应用格子Boltzmann方法(LBM),实现了流体在二维1:3扩张流道及3:1收缩流道中流动的数值模拟,获得了黏弹性流体在扩张和收缩流道中的流场分布.结合颗粒的受力和运动规则,基于点源颗粒模型,数值分析了颗粒在扩张流和收缩流中的沉降过程和特征,讨论了颗粒相对质量和起始位置以及雷诺数Re和威森伯格数Wi对颗粒沉降特征的影响.结果表明,颗粒相对质量和起始位置以及Re对颗粒沉降轨迹和落点影响较大,而Wi的影响则较小.  相似文献   

17.
双圆柱绕流特性的模拟研究   总被引:1,自引:0,他引:1  
采用格子Boltzmann方法对低雷诺数下气体绕流圆柱的规律进行了研究. 对比计算了双 圆柱在不同圆心距、不同Re数、不同来流速度与双圆柱圆心连线角度的情况下,各个圆柱的 受力大小和曳力系数. 结果表明,若Re数为20, 改变圆柱间距,圆柱间距在1.2d和1.4d 之间时,下游圆柱所受曳力有极小值;双圆柱间距为1.6d时,双圆柱受到总曳力最小;圆 柱间距大于2d时,上游颗粒受到的曳力不再受到下游颗粒的影响. 若圆柱间距 为1.2d, 改变雷诺数,Re数在30和40之间,下游圆柱所受曳力有极小值. 另外, 来流速度角度对圆柱的受力影响很大. 上述规律为低Re数下圆柱绕流的深入研究 与应用打下基础.  相似文献   

18.
To simulate turbulent flow over a rough wall without resolving complicated rough geometries, a macroscopic rough wall model is developed based on spatial (plane) averaging theory. The plane-averaged drag force term, which arises through averaging the Navier–Stokes equations in a plane parallel to a rough wall, can be modeled using a plane porosity and a plane hydraulic diameter. To evaluate the developed model, direct and macroscopic model simulations for turbulence over irregularly distributed semi-spheres at Reynolds number of 300 are carried out using the D3Q27 multiple-relaxation time lattice Boltzmann method. The results show that the developed model can be used to predict rough wall skin friction. The results agree quantitatively with standard turbulence statistics such as mean velocity and Reynolds stress profiles with the fully resolved DNS data. Since velocity dispersion occurs inside the rough wall and is found to contribute to turbulence energy dissipation, which the developed model cannot account for, the developed model fails to reproduce dispersion-related turbulence energy dissipation. However, it is found that the plane-averaged drag force term can successfully recover the deficiency of dispersion-related turbulence energy dissipation.  相似文献   

19.
We perform direct numerical simulation of three‐dimensional turbulent flows in a rectangular channel, with a lattice Boltzmann method, efficiently implemented on heavily parallel general purpose graphical processor units. After validating the method for a single fluid, for standard boundary layer problems, we study changes in mean and turbulent properties of particle‐laden flows, as a function of particle size and concentration. The problem of physical interest for this application is the effect of water droplets on the turbulent properties of a high‐speed air flow, near a solid surface. To do so, we use a Lagrangian tracking approach for a large number of rigid spherical point particles, whose motion is forced by drag forces caused by the fluid flow; particle effects on the latter are in turn represented by distributed volume forces in the lattice Boltzmann method. Results suggest that, while mean flow properties are only slightly affected, unless a very large concentration of particles is used, the turbulent vortices present near the boundary are significantly damped and broken down by the turbulent motion of the heavy particles, and both turbulent Reynolds stresses and the production of turbulent kinetic energy are decreased because of the particle effects. We also find that the streamwise component of turbulent velocity fluctuations is increased, while the spanwise and wall‐normal components are decreased, as compared with the single fluid channel case. Additionally, the streamwise velocity of the carrier (air) phase is slightly reduced in the logarithmic boundary layer near the solid walls. Copyright © 2015 John Wiley & Sons, Ltd.  相似文献   

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