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Impact of Turbulence Models and Shape Parameterization on Robust Aerodynamic Shape Optimization

机译:湍流模型和形状参数化对鲁棒空气动力学形状优化的影响

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摘要

The objective of this paper is to investigate the impact of two commonly used turbulence models with three different shape parameterization techniques in Reynolds-averaged Navier-Stokes simulations on two-dimensional optimum design obtained with gradient-based deterministic and robust aerodynamic shape optimization in transonic, viscous, turbulent flow. The main contribution of this study to aerodynamic design area is to evaluate the impact of turbulence models and shape parameterization techniques on the computational cost, optimal shape, and its performance obtained with robust optimization under uncertainty. The two turbulence models investigated include Spalart-Allmaras and Menter's shear-stress transport models. Hicks-Henne bump functions, B-spline curves, and free-form deformation are used as shape parameterization techniques. The results of the current study show that the shape parameterization technique has a larger impact on the computational cost compared to the turbulence model in both deterministic and robust design. Robust design tends to reduce the impact of the turbulence model selection on the optimum shape and performance, whereas the turbulence model becomes important for the deterministic design at off-design conditions. In this study, the robustness of the final design obtained with stochastic optimization approach is also demonstrated over the Mach number range considered as the uncertain operating condition.
机译:本文的目的是研究雷诺平均Navier-Stokes模拟中两个具有三种不同形状参数化技术的常用湍流模型对基于跨音速的基于梯度的确定性和鲁棒空气动力学形状优化所获得的二维最优设计的影响,粘性,湍流。这项研究对空气动力学设计领域的主要贡献是评估湍流模型和形状参数化技术对计算成本,最佳形状及其在不确定性下通过鲁棒优化获得的性能的影响。研究的两个湍流模型包括Spalart-Allmaras和Menter的切应力传递模型。 Hicks-Henne凹凸函数,B样条曲线和自由形式的变形用作形状参数化技术。当前的研究结果表明,在确定性和鲁棒性设计中,与湍流模型相比,形状参数化技术对计算成本的影响更大。健壮的设计趋于减少湍流模型选择对最佳形状和性能的影响,而湍流模型对于非设计条件下的确定性设计至关重要。在这项研究中,通过随机优化方法获得的最终设计的鲁棒性也被证明在被视为不确定操作条件的马赫数范围内。

著录项

  • 来源
    《Journal of Aircraft》 |2019年第3期|1099-1115|共17页
  • 作者单位

    Missouri Univ Sci & Technol, Dept Aerosp & Mech Engn, Rolla, MO 65409 USA;

    Missouri Univ Sci & Technol, Dept Aerosp & Mech Engn, Aerosp Engn, Rolla, MO 65409 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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