共查询到17条相似文献,搜索用时 46 毫秒
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采用理论分析和数值模拟相结合的方法,系统研究了尺度自适应模拟(scale-adaptive simulation,SAS)和大涡模拟(large-eddy simulation,LES)的关联性问题.在理论分析方面,对比分析了系综平均和滤波的定义、Spalart-Allmaras(SA)湍流模型和动态亚格子(subgrid-scale,SGS)模型关于湍流黏性系数的求解方式.理论分析结果表明,系综平均等价于盒式直接滤波,SAS和LES的控制方程在数学形式上具有一致性;SAS存在过多的湍流耗散,主要来自于SA输运方程中的扩散项.在数值模拟方面,选取来流Mach数0.55,Reynolds数2×105的圆柱可压缩绕流为分析算例.计算结果表明,SAS和LES预测的大尺度平均流场信息几乎一致,SAS预测的湍流脉动信息略低于LES.SAS在圆柱近尾迹区的湍流耗散过大,而在稍远的尾迹区几乎能够完全等效于LES. 相似文献
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湍流边界层流动是一种广泛存在于飞行器内部和外部的流动现象,是基础理论和模型验证的重要研究对象.能够捕捉大部分流动细节且计算量适中的大涡模拟(large-eddy simulation,LES)方法在湍流数值模拟中得到了越来越广泛的应用.文章基于格心有限差分方法,使用4阶紧致中心格式离散N-S方程无黏项,分别应用5种不同的亚格子(subgrid-scale,SGS)模型,即隐式,SM(Smagorinsky model),DSM(dynamic Smagorinsky model),WALE(wall-adapting local eddy-viscosity model)和CSM(coherent structures model),对Re = 3 000,Ma = 0.5的等温壁面槽道流动进行了大涡模拟研究.与实验值和直接数值模拟(direct numerical simulation,DNS)结果对比后发现,流场平均温度、平均密度等热力学量以及平均流向速度对亚格子模型不敏感,不适宜作为判断模型优劣的判据.亚格子模型在壁面附近的耗散越大,壁面摩擦速度以及阻力系数就越小.对于与速度相关的脉动量来说,不同模型得到的结果在壁面和脉动峰值附近误差比较大,中心线附近较小;显式模型结果在流向速度峰值处均高于参考值,而在展向和壁面法向速度脉动峰值处则均偏低.考虑显式的4种模型在壁面附近的涡黏系数分布,DSM和CSM曲线满足涡黏系数与无量纲壁面距离3次方成正比的分布规律,SM曲线斜率偏小而WALE曲线斜率偏大. 相似文献
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基于Smagorinsky涡黏模型以及颗粒动理学理论,建立了气固两相流双大涡模拟模型。考虑大涡模拟中过滤尺度的影响,给出颗粒相亚格子压力和热传导系数计算模型。考虑颗粒聚团对两相作用的影响,给出了考虑颗粒聚团作用的气固两相多尺度曳力系数模型。数值模拟了提升管内气固两相流动特性,合理地预测出了提升管内气固两相环-核流动结构。模拟结果与Knowlton等实测结果相吻合。 相似文献
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在多重网格驱动的,高效且得到充分验证的有限体积方法的基础上发展了可压缩流大涡模拟的方法.空间离散采用Jameson的中心格式附加二阶和四阶耗散的方法,时间推进则采用了双时间步长的方法.亚格子剪切应力张量和亚格子热通量用Smagorinsky模型进行模拟.通过对各向同性紊流能量衰减的模拟来验证本方法的准确性和高效性,模拟得到的能量谱和紊流动能衰减历程与过滤后的CBC实验数据吻合良好. 相似文献
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Amin Rasam Stefan Wallin Geert Brethouwer Arne V. Johansson 《Journal of Turbulence》2013,14(11):752-775
We analyse the performance of the explicit algebraic subgrid-scale (SGS) stress model (EASSM) in large eddy simulation (LES) of plane channel flow and the flow in a channel with streamwise periodic hill-shaped constrictions (periodic hill flow) which induce separation. The LESs are performed with the Code_Saturne which is an unstructured collocated finite volume solver with a second-order spatial discretisation suitable for LES of incompressible flow in complex geometries. At first, performance of the EASSM in LES of plane channel flow at two different resolutions using the Code_Saturne and a pseudo-spectral method is analysed. It is observed that the EASSM predictions of the mean velocity and Reynolds stresses are more accurate than the conventional dynamic Smagorinsky model (DSM). The results with the pseudo-spectral method were, in general, more accurate. In the second step, LES with the EASSM of flow separation in the periodic hill flow is compared to LES with the DSM, no SGS model and a highly resolved LES data using the DSM. Results show that the mean velocity profiles, the friction and pressure coefficients, the length and shape of the recirculation bubble, as well as the Reynolds stresses are considerably better predicted by the EASSM than the DSM and the no SGS model simulations. It was also observed that in some parts of the domain, the resolved strain-rate and SGS shear stress have the same sign. The DSM cannot produce a correct SGS stress in this case, in contrast to the EASSM. 相似文献
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J. Graham K. Kanov X. I. A. Yang M. Lee N. Malaya C. C. Lalescu 《Journal of Turbulence》2016,17(2):181-215
The output from a direct numerical simulation (DNS) of turbulent channel flow at Reτ ≈ 1000 is used to construct a publicly and Web services accessible, spatio-temporal database for this flow. The simulated channel has a size of 8πh × 2h × 3πh, where h is the channel half-height. Data are stored at 2048 × 512 × 1536 spatial grid points for a total of 4000 time samples every 5 time steps of the DNS. These cover an entire channel flow-through time, i.e. the time it takes to traverse the entire channel length 8πh at the mean velocity of the bulk flow. Users can access the database through an interface that is based on the Web services model and perform numerical experiments on the slightly over 100 terabytes (TB) DNS data on their remote platforms, such as laptops or local desktops. Additional technical details about the pressure calculation, database interpolation, and differentiation tools are provided in several appendices. As a sample application of the channel flow database, we use it to conduct an a-priori test of a recently introduced integral wall model for large eddy simulation of wall-bounded turbulent flow. The results are compared with those of the equilibrium wall model, showing the strengths of the integral wall model as compared to the equilibrium model. 相似文献