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A new methodology for the numerical simulation of wall bounded turbulent flows.

机译:一种新的数值方法,用于数值模拟壁面湍流。

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Research is presented on the development and testing of a new procedure for the time dependent, spatially varying numerical simulation of wall bounded turbulent flows. The Flow Simulation Methodology (FSM), as it is now known, was originally proposed by Speziale (1996a) for the purpose of computing complex, non-equilibrium flows which are currently beyond the reach of Smagorinsky based Large-Eddy Simulations (LES). The new method represents a hybrid approach that combines favorable aspects of Reynolds stress modeling [used for Reynolds Averaged Navier-Stokes (BANS) calculations] with the underlying principles of LES. For instance, Reynolds stress models developed for non-equilibrium, anisotropic, and/or rotational flows can be utilized in the unsteady manner of LES, i.e. where the flow field is decomposed into resolved-scale (calculated) and subgrid-scale (modeled) components, thereby reducing computational requirements. The key to the FSM is a contribution function which provides a degree of local turbulence modeling that is dependent upon the ratio of the numerical resolution to the Kolmogorov length-scale, an estimate for the smallest scales of turbulent motion. With this approach, a calculation resolved to the level of a Direct Numerical Simulation (DNS) can proceed continuously to a Reynolds Averaged Navier-Stokes calculation as the numerical resolution is decreased and/or the Reynolds number is increased. In between these two limits, an “untraditional” LES is recovered. The method is untraditional because it replaces the commonly employed Smagorinsky subgrid-scale model, which is known to have considerable limitations, with a more capable Reynolds stress model.; A detailed evaluation of the Flow Simulation Methodology is made for the test case of a transitional and turbulent flat plate boundary layer with zero pressure gradient. The relatively simple geometry is chosen because the technical issues associated with combining elements of RANS calculations and LES must be established and the FSM itself must be validated before more complex flows can be attempted. The Reynolds stresses needed for the new method are computed using the two-equation Algebraic Stress Model (ASM) of Gatski & Speziale (1993) developed for non-equilibrium turbulent flows. Results of FSM calculations are compared with results obtained from coarse grid DNS, traditional LES based on the Smagorinsky subgrid-scale model, and RANS, all of which are implemented using an identical core computer code. This approach is extremely valuable to the evaluation of the FSM since a common code allows for certain behaviors to be more easily attributed to the turbulence models as opposed to numerical effects. Further validation is achieved through comparisons of FSM results with various direct numerical simulations and experiments available in the literature.
机译:提出了开发和测试一种新方法的研究,该方法用于对与时间有关的,空间受限的壁边界湍流进行数值模拟。众所周知,流动模拟方法学(FSM)最初是由Speziale(1996 a )提出的,其目的是计算目前基于Smagorinsky无法实现的复杂,非平衡流大涡模拟(LES)。新方法代表了一种混合方法,该方法结合了雷诺应力模型(用于雷诺平均Navier-Stokes(BANS)计算)的有利方面与LES的基本原理。例如,针对非平衡,各向异性和/或旋转流开发的雷诺应力模型可以以LES的不稳定方式使用,即将流场分解为分辨尺度(计算得出)和亚网格尺度(建模)时组件,从而减少了计算需求。 FSM的关键是贡献函数,该函数提供一定程度的局部湍流建模,该建模过程取决于数值分辨率与Kolmogorov长度尺度的比率(最小湍流尺度的估计)。通过这种方法,随着数值分辨率的降低和/或雷诺数的增加,解析为直接数值模拟(DNS)级别的计算可以连续进行雷诺平均Navier-Stokes计算。在这两个极限之间,恢复了“非传统” LES。该方法是非传统的,因为它用功能更强大的雷诺应力模型代替了众所周知的局限性的Smagorinsky子网格规模模型。针对带有零压力梯度的过渡湍流平板边界层的测试案例,对流动模拟方法进行了详细评估。选择相对简单的几何形状是因为必须确定与RANS计算和LES的组合元素相关的技术问题,并且必须先验证FSM本身,然后才能尝试更复杂的流程。新方法所需的雷诺应力是使用为非平衡湍流开发的Gatski&Speziale(1993)的两方程式代数应力模型(ASM)计算的。将FSM计算的结果与从粗网格DNS,基于Smagorinsky子网格规模模型的传统LES和RANS获得的结果进行比较,所有这些都使用相同的核心计算机代码实现。这种方法对于FSM的评估非常有价值,因为通用代码允许将某些行为更容易地归因于湍流模型,而不是数值效应。通过将FSM结果与文献中提供的各种直接数值模拟和实验进行比较,可以进一步验证。

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