Mesh and model requirements for capturing deep-stall aerodynamics in low-Mach-number flows

IF 1.5 4区 工程技术 Q3 MECHANICS Journal of Turbulence Pub Date : 2023-06-14 DOI:10.1080/14685248.2023.2225141
S. Bidadi, G. Vijayakumar, Ashesh Sharma, M. Sprague
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Abstract

The paper presents a comprehensive computational fluid dynamics investigation of the effects of grid resolution and turbulence-model choice for capturing the unsteady three-dimensional aerodynamic performance of NACA 0012 and 0021 airfoils, with specific focus on the deep-stall regime. At high angles of attack (α), wind turbine blades routinely experience vortex-induced vibrations, which can cause significant structural damages. Accurate predictions of post-stall aerodynamics can identify the frequencies at which such vibrations maybe triggered. In this context, the NACA 0012 airfoil simulations are conducted at a chord-based Reynolds number, , with the k-ω Shear-Stress Transport Reynolds-Averaged Navier-Stokes (RANS) and Improved Delayed Detached Eddy Simulation (IDDES) hybrid RANS-Large Eddy Simulation turbulence models. The effect of mesh resolution both in the wall-normal and spanwise directions is investigated. Only the IDDES model with a minimum spanwise resolution of 24 cells per chord length correctly predicts the aerodynamic forces. Spectral analysis shows the peak primary shedding frequency at , which signifies the end of the stall region. In the post-stall regime, both lift and drag frequencies drop asymptotically with increasing α. The Strouhal number, based on normalised chord length, remains nearly constant in this region. Based on this study, NACA 0021 airfoil runs are performed with IDDES for and on the finest wall-normal mesh and three spanwise grids. Simulations conducted on the finer spanwise grids demonstrate grid independence and show good agreement with experiments. The effect of varying on the airfoil frequency statistics is investigated. Additionally, comparison studies are presented to investigate the impact of airfoil thickness on the frequency content at . The results from the study provide guidance on the choice of mesh resolution with the IDDES model to accurately capture aerodynamic quantities for complex industrial applications.
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低马赫数流中捕获深失速空气动力学的网格和模型要求
本文对网格分辨率和湍流模型选择的影响进行了全面的计算流体动力学研究,以捕捉NACA 0012和0021翼型的非定常三维气动性能,特别是深失速状态。在高攻角(α)下,风力涡轮机叶片通常会经历涡流引起的振动,这可能会导致严重的结构损伤。对失速后空气动力学的准确预测可以确定可能触发这种振动的频率。在这种情况下,NACA 0012翼型模拟是在基于弦的雷诺数下进行的,采用k-ω剪切应力输运雷诺平均纳维-斯托克斯(RANS)和改进的延迟分离涡模拟(IDDES)混合RANS大涡模拟湍流模型。研究了网格分辨率在墙法线方向和跨度方向上的影响。只有最小展向分辨率为每弦长24个单元的IDDES模型才能正确预测空气动力。频谱分析显示了处的峰值初级脱落频率,这表示失速区域的结束。在失速后状态下,升力和阻力频率都随着α的增加而渐近下降。基于归一化弦长的斯特劳哈尔数在该区域几乎保持不变。基于这项研究,NACA 0021翼型在最细的壁面法向网格和三个展向网格上使用IDDES进行了运行。在更精细的展向网格上进行的模拟表明了网格的独立性,并与实验显示出良好的一致性。研究了变化对翼型频率统计的影响。此外,还进行了比较研究,以研究翼型厚度对频率含量的影响。研究结果为IDDES模型的网格分辨率选择提供了指导,以准确捕捉复杂工业应用中的空气动力学量。
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来源期刊
Journal of Turbulence
Journal of Turbulence 物理-力学
CiteScore
3.90
自引率
5.30%
发文量
23
审稿时长
6-12 weeks
期刊介绍: Turbulence is a physical phenomenon occurring in most fluid flows, and is a major research topic at the cutting edge of science and technology. Journal of Turbulence ( JoT) is a digital forum for disseminating new theoretical, numerical and experimental knowledge aimed at understanding, predicting and controlling fluid turbulence. JoT provides a common venue for communicating advances of fundamental and applied character across the many disciplines in which turbulence plays a vital role. Examples include turbulence arising in engineering fluid dynamics (aerodynamics and hydrodynamics, particulate and multi-phase flows, acoustics, hydraulics, combustion, aeroelasticity, transitional flows, turbo-machinery, heat transfer), geophysical fluid dynamics (environmental flows, oceanography, meteorology), in physics (magnetohydrodynamics and fusion, astrophysics, cryogenic and quantum fluids), and mathematics (turbulence from PDE’s, model systems). The multimedia capabilities offered by this electronic journal (including free colour images and video movies), provide a unique opportunity for disseminating turbulence research in visually impressive ways.
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