...
首页> 外文期刊>Open Journal of Fluid Dynamics >Tracking a Tip Vortex with Adaptive Vorticity Confinement and Hybrid RANS-LES
【24h】

Tracking a Tip Vortex with Adaptive Vorticity Confinement and Hybrid RANS-LES

机译:利用自适应涡度限制和混合RANS-LES跟踪尖端涡旋

获取原文
           

摘要

The prediction of coherent vortices with standard RANS solvers suffers especially from discretisation and modelling errors which both introduce numerical diffusion. The adaptive Vorticity Confinement (VC) method targets to counteract one part of the discretisation error: the one due to the discretisation of the convection term. This method is applied in conjunction with a hybrid RANS-LES turbulence model to overcome the overprediction of turbulence intensity inside vortex cores which is a typical deficiency of common RANS solvers. The third main source for numerical diffusion originates from the spatial discretisation of the solution domain in the vicinity of the vortex core. The corresponding error is analysed within a grid convergence study. A modification of the adaptive VC method used in conjunction with a high-order discretisation of the convection term is presented and proves to be superior. The simulations of a wing tip vortex flow are validated in terms of vortex velocity profiles using the results of a wind tunnel experiment performed by Devenport and colleagues (1996). Besides, the results are compared with another numerical study by Wells (2009) who uses a Reynolds Stress turbulence model. It turns out that the application of the modified adaptive VC method on the one hand reinforces the tip vortex, and on the other hand accelerates the axial flow which leads to a slight degradation compared to the experimental results. The result of Wells is more accurate close to the wing, but the result obtained here is superior further downstream as no excessive diffusion of the tip vortex occurs.
机译:使用标准RANS求解器进行相干涡旋的预测尤其会受到离散化和建模误差的影响,这两者都会引入数值扩散。自适应涡度限制(VC)方法旨在抵消离散化误差的一部分:由于对流项离散化而引起的误差。该方法与混合的RANS-LES湍流模型结合使用,克服了涡流核内部湍流强度的过高预测,这是常见RANS求解器的典型缺陷。数值扩散的第三个主要来源是漩涡核心附近溶液域的空间离散化。在网格收敛研究中分析了相应的误差。提出了与对流项的高阶离散化结合使用的自适应VC方法的一种改进,并被证明是更好的。利用Devenport及其同事(1996)进行的风洞实验的结果,根据涡旋速度分布图验证了翼尖涡旋流动的模拟。此外,将结果与Wells(2009)使用雷诺应力湍流模型的另一项数值研究进行了比较。事实证明,改进的自适应VC方法的应用一方面会增强尖端涡流,另一方面会加速轴向流,与实验结果相比,轴向流会稍有下降。 Wells的结果在靠近机翼的位置更准确,但此处获得的结果在下游更佳,因为不会发生尖端涡旋的过度扩散。

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