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Grid-Adapted FUN3D Computations for the Second High-Lift Prediction Workshop

机译:第二届高空预报研讨会的网格自适应FUN3D计算

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摘要

Contributions of the unstructured Reynolds-averaged Navier-Stokes code FUN3D to the 2nd AIAA Computational Fluid Dynamics High-Lift Prediction Workshop are described, and detailed comparisons are made with experimental data. Using workshop-supplied grids, FUN3D results for the simplified high-lift configuration are compared with results from the structured code CFL3D. Using the same turbulence model, both codes compare reasonably well in terms of total forces and moment, and the maximum lift is similarly over-predicted for both codes compared to experiment. By including more representative geometry features such as slat and flap support brackets and slat pressure tube bundles, FUN3D captures the general effects of the Reynolds number variation, but under-predicts maximum lift on workshop-supplied grids in comparison with the experimental data due to excessive separation. However, when output-based, off-body grid adaptation in FUN3D is employed, results improve considerably. In particular, when the geometry includes both brackets and the pressure tube bundles, grid adaptation results in a more accurate prediction of lift near stall in comparison with the wind-tunnel data. Furthermore, a rotation-corrected turbulence model shows improved pressure predictions on the outboard span when using adapted grids.
机译:描述了非结构化雷诺平均Navier-Stokes代码FUN3D对第二届AIAA计算流体动力学高空预测研讨会的贡献,并与实验数据进行了详细的比较。使用车间提供的网格,将简化的高举配置的FUN3D结果与结构化代码CFL3D的结果进行比较。使用相同的湍流模型,两个代码在总力和力矩方面进行了比较合理的比较,与实验相比,两个代码的最大升程同样被过度预测。通过包括更具代表性的几何特征,例如板条和襟翼支撑架以及板条压力管束,FUN3D捕获了雷诺数变化的一般影响,但由于过多的实验数据,与实验数据相比,它低估了车间提供的网格的最大升力分离。但是,当在FUN3D中采用基于输出的体外网格自适应时,结果会大大提高。尤其是,当几何结构同时包括支架和压力管束时,与风洞数据相比,网格自适应可以更准确地预测失速附近的升力。此外,当使用自适应网格时,旋转校正的湍流模型在外侧跨度上显示出改进的压力预测。

著录项

  • 来源
    《Journal of Aircraft 》 |2015年第4期| 1098-1111| 共14页
  • 作者单位

    NASA Langley Res Ctr, Computat AeroSci Branch, Hampton, VA 23681 USA;

    NASA Langley Res Ctr, Computat AeroSci Branch, Hampton, VA 23681 USA;

    NASA Langley Res Ctr, Computat AeroSci Branch, Hampton, VA 23681 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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