In order to achieve a virtual certification process and robust designs for turbomachinery, the uncertainty bounds for computational fluid dynamics have to be known. The formulation of turbulence closure models implies a major source of the overall uncertainty of Reynold-averaged Navier Stokes simulations. We discuss the common practice of applying a physics constrained eigenspace perturbation of the Reynolds stress tensor in order to account for the model form uncertainty of turbulence models. Since the basic methodology often leads to generous uncertainty estimates, we extend a recent approach of adding a machine learning strategy. The application of a data-driven method is motivated by striving for the detection of flow regions, which are prone to suffer from a lack of turbulence model prediction accuracy. In this way any user input related to choosing the degree of uncertainty is supposed to become obsolete. This work especially investigates an approach, which tries to determine an a priori estimation of prediction confidence, when there is no accurate data available to judge the prediction. The flow around the NACA 4412 airfoil at near-stall conditions serves to demonstrate the successful application of the data-driven eigenspace perturbation framework. We especially highlight the objectives and limitations of the underlying methodology finally.
翻译:为了实现虚拟认证过程和涡轮机械的稳健设计,必须了解计算流动态的不确定性界限。制定动荡封闭模型意味着Reynold平均纳维埃斯托克斯模拟的整体不确定性的主要来源。我们讨论了对Reynolds压力施压进行物理限制天体扰动的常见做法,以便考虑到气旋模型的模型形式不确定性。由于基本方法往往导致慷慨的不确定性估计,我们推广了最近增加机器学习战略的方法。数据驱动方法的应用是为了探测流区域,因为流区域容易因动荡模型预测的准确性而受到影响。这样,与选择不确定性程度有关的任何用户投入就应该过时。这项工作特别调查了一种办法,即当没有准确的数据来判断预测时,试图确定对预测信心的预先估计。在接近停滞条件下的NACA 4412空气流,有助于显示数据驱动空间渗透框架的成功应用。我们特别强调了最终目标以及基本方法的局限性。