首页> 外文会议>AIAA SciTech forum;AIAA Aerospace Sciences Meeting >Prediction of Turbulent Secondary Flows in Ducts Using Equilibrium Wall-Modeled LES
【24h】

Prediction of Turbulent Secondary Flows in Ducts Using Equilibrium Wall-Modeled LES

机译:使用平衡壁模型LES预测管道中的湍流二次流

获取原文

摘要

For many practical applications, large eddy simulation (LES) and direct numerical simulation (DNS) are still too computationally expensive to be viable engineering tools. By modeling the small scales within the boundary layer, wall-modeled LES (WMLES) reduces this cost and enables high Reynolds number calculations. For a WMLES approach that relies on the assumption of an equilibrium boundary layer, however, a primary concern is the extent to which the set of simplified equations solved by the wall-model may be insufficient to predict boundary layer separation or three-dimensional behavior. Additionally, most equilibrium WMLES approaches rely on some type of eddy viscosity term to parameterize the effects of unresolved turbulence near the wall. In many flows of interest, however, the anisotropy of the Reynolds stress tensor violates the assumptions inherent to the most common eddy viscosity models. Hence, the accuracy of WMLES for these types of flows is not yet fully established. This research attempts to identify some of the potential deficiencies in the equilibrium WMLES methodology for turbulent flows through non-circular ducts and demonstrates how certain straightforward modifications can significantly improve the calculation of shear stress. The shear stress distributions are then shown to be influential in the development of the secondary vortices which can significantly alter the primary, axial flow. Several model variations are initially evaluated using two streamwise-periodic, incompressible test cases before being applied to a spatially-evolving, compressible flow. These modifications are shown to improve the prediction of the secondary flows found in turbulent ducts across a range of Reynolds and Mach numbers.
机译:对于许多实际应用而言,大涡模拟(LES)和直接数值模拟(DNS)仍然在计算上过于昂贵,无法成为可行的工程工具。通过对边界层内的小比例尺进行建模,墙面建模的LES(WMLES)降低了成本,并实现了高雷诺数计算。但是,对于依赖于平衡边界层假设的WMLES方法,主要关注的是在多大程度上壁模型求解的简化方程组可能不足以预测边界层分离或三维行为。此外,大多数平衡WMLES方法都依赖某种类型的涡流粘度项来参数化壁附近未解决的湍流的影响。然而,在许多感兴趣的流中,雷诺应力张量的各向异性违反了最常见的涡流粘度模型固有的假设。因此,针对这些类型的流的WMLES的准确性尚未完全确定。这项研究试图找出通过非圆形管道的湍流的平衡WMLES方法中的某些潜在缺陷,并证明某些简单的修改如何可以显着改善剪切应力的计算。然后显示出剪切应力分布对次级涡旋的发展有影响,次级涡旋的发展会显着改变初级轴向流动。首先使用两个流周期不可压缩的测试用例对几种模型变化进行评估,然后再应用于空间演化的可压缩流。显示了这些修改可以改善对在一系列雷诺数和马赫数范围内的湍流导管中发现的二次流的预测。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号