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The large-eddy simulation of incompressible flows in simple and complex geometries.

机译:在简单和复杂几何中不可压缩流的大涡模拟。

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A large-eddy simulation methodology (LES) has been developed for predicting the turbulent physics of an incompressible flow in simple and complex geometries. The Cartesian form of the governing equations was first verified, and then later used to investigate a three-dimensional shear-driven cavity flow. The investigation involved Reynolds numbers of 2000, 3200, 5000 and 10000 and focused on the unsteadiness and turbulent characteristics of the flow. At the low Reynolds numbers (Re {dollar}le{dollar} 5000) where the cavity flow is fully laminar, direct numerical simulations (DNS) were conducted whereas the LES methodology was adopted to predict the cavity flow at the higher Reynolds number (Re = 10000). Determining the parameters in the damped subgrid scale (SGS) turbulence model for this complex flow was guided by the DNS results at Re = 5000. The SGS model was also verified against DNS results at Re = 7500 where the cavity flow was known through laboratory experimentation to be locally transitional. The LES results using the damped SGS model verified the published experimental evidence as well as uncovered new flow features within the cavity.; LES computations were also carried-out of the three-dimensional shear-driven cavity flow at a high Reynolds number where the SGS turbulent field was represented by a dynamic model. Lilly's least-squares expression was tested for determining Smagorinsky's coefficient in the model without ad hoc measures such as ensemble-averaging or filtering. However, zero cutoff of negative total viscosity (kinematic plus turbulent eddy viscosity) was necessary to maintain stable solutions. A discretized filter function was derived for the test filter. Both qualitative and quantitative comparisons to experimental data show that the dynamic model performed quite well. The dynamic model gave better comparisons to the experimental evidence than the damped model did.; Vortex formation in the wake of a circular cylinder and their subsequent downstream transport was also numerically investigated by LES. Here however, the curvilinear form of the governing equations was necessary to perform the computations. A new generalized dynamic model was derived to represent the SGS stress field in the curvilinear space. This new model introduced the contravariant velocity components as part of the field variables. New downstream boundary conditions were also formulated to permit the shed vortices to exit with minimum disturbance. The focus of the investigation was at Re = 5600 with some verification of the computations at Re = 200 and Re = 3000. At all of these Reynolds numbers, the upstream boundary layer was laminar but the wake was fully turbulent at Re = 3000 and Re = 5600. The LES results of the many interesting characteristics of the wake showed good comparisons to the experimental data.
机译:已经开发出大涡模拟方法(LES),以预测简单和复杂几何形状中不可压缩流的湍流物理学。首先验证了控制方程的笛卡尔形式,然后将其用于研究三维剪切驱动型腔流。研究涉及雷诺数分别为2000、3200、5000和10000,并着眼于流动的不稳定和湍流特性。在低雷诺数(Re {dollar} le {dollar} 5000)下,其中腔流是完全层流的,进行了直接数值模拟(DNS),而采用LES方法预测了更高雷诺数(Re = 10000)。在Re = 5000时的DNS结果指导下,在阻尼子网格尺度(SGS)湍流模型中确定参数。在Re = 7500时,也针对DNS结果对SGS模型进行了验证,在Re = 7500时,通过实验室实验可以知道空腔流量是局部过渡的。使用阻尼SGS模型的LES结果验证了已发表的实验证据以及在腔体内未发现的新流动特征。 LES计算还以高雷诺数进行了三维剪切驱动腔流,其中SGS湍流场由动态模型表示。测试了Lilly的最小二乘表达式,以确定模型中的Smagorinsky系数,而无需进行总体平均或滤波等临时措施。但是,为了保持稳定的溶液,负总粘度(运动加湍流涡流粘度)的零截止是必需的。为测试滤波器导出了离散滤波器函数。与实验数据的定性和定量比较均表明,该动态模型表现良好。动态模型比阻尼模型更好地与实验证据进行了比较。 LES还对圆柱尾流中的涡旋形成及其随后的下游传输进行了数值研究。但是,在这里,控制方程的曲线形式是执行计算所必需的。推导了一个新的广义动力学模型来表示曲线空间中的SGS应力场。这个新模型引入了反速度分量作为场变量的一部分。还制定了新的下游边界条件,以使脱落的涡流以最小的干扰退出。研究的重点是Re = 5600,并对Re = 200和Re = 3000的计算进行了一些验证。在所有这些雷诺数下,上游边界层都是层流的,但是尾波在Re = 3000和Re时完全湍流=5600。尾流的许多有趣特征的LES结果与实验数据进行了很好的比较。

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