Numerical Investigation of a Simplified Wing–body Junction Flow

IF 1.3 4区 工程技术 Q4 MECHANICS International Journal of Computational Fluid Dynamics Pub Date : 2022-09-14 DOI:10.1080/10618562.2022.2162892
Zi-Qiao Wei, J. Li, Songxiang Tang
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Abstract

The flow past a simplified wing-body junction configuration is simulated using a shear layer adaptive improved delayed detached-eddy-simulation (SLA-IDDES) approach in which an appropriate subgrid lengthscale is adopted in the boundary region, where the grid may be strongly anisotropic, to prevent the excessive generation of subgrid-scale eddy viscosity. The numerical results show overall good agreement with the experiment carried out by Ölçmen and Simpson. The self-induced chaotic switching of the horseshoe vortex between two flow modes is simulated and analysed, and its effects on the vortex legs and their inherent oscillation are also investigated. It is found that the corner vortex also exhibits an alternating formation and breakdown process with basically the same frequency as the horseshoe vortex. Corner separation is found to be affected also by the upstream horseshoe vortex and the inherent oscillation of the vortex legs.
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简化翼-体结合部流动的数值研究
采用剪切层自适应改进延迟分离涡模拟(SLA-IDDES)方法模拟经过简化翼身结合部结构的流动,该方法在网格可能具有强各向异性的边界区域采用适当的亚网格长度尺度,以防止亚网格尺度涡流粘度的过度产生。数值计算结果与Ölçmen和Simpson的实验结果基本一致。模拟和分析了马蹄涡在两种流动模式之间的自生混沌切换,并研究了其对涡腿及其固有振荡的影响。结果表明,角涡也表现出与马蹄形涡频率基本相同的交替形成和击穿过程。研究发现,上游的马蹄形涡和涡腿的固有振荡也会对角分离产生影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
2.70
自引率
7.70%
发文量
25
审稿时长
3 months
期刊介绍: The International Journal of Computational Fluid Dynamics publishes innovative CFD research, both fundamental and applied, with applications in a wide variety of fields. The Journal emphasizes accurate predictive tools for 3D flow analysis and design, and those promoting a deeper understanding of the physics of 3D fluid motion. Relevant and innovative practical and industrial 3D applications, as well as those of an interdisciplinary nature, are encouraged.
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