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Kriging-model-based uncertainty quantification in computational fluid dynamics

机译:计算流体力学中基于Kriging模型的不确定性量化

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This paper proposes an efficient and accurate non-intrusive uncertainty quantification (UQ) method in computational fluid dynamics (CFD). Emphasis is placed on developing an UQ method that can accurately predict stochastic behaviors of output solution with small number of sampling simulations, and is also accurate for non-smooth output uncertainty responses. The proposed method is based on Kriging surrogate model, and the Kriging function values are used to evaluate output uncertainties robustly even with non-smooth responses, while using both the fit uncertainty and the gradient information of the Kriging predictors for dynamic adaptive sampling. The proposed Kriging-model-based UQ method shows a superior performance in estimating the non-smooth responses of output solution in terms of accuracy and robustness compared to the existing polynomial chaos expansion and the adaptive sampling method based on only the Kriging predictor fit uncertainty. The proposed method is first tested on analytical non-smooth functions under uniform uncertainties, and then applied to the transonic RAE 2822 airfoil flow under normal uncertainties in freestream Mach number by coupling the proposed UQ method with CFD.
机译:本文提出了一种高效,准确的计算流体力学(CFD)中的非侵入式不确定性量化(UQ)方法。重点在于开发一种UQ方法,该方法可以通过少量采样仿真来准确预测输出解决方案的随机行为,并且对于非平滑的输出不确定性响应也很准确。所提出的方法基于Kriging替代模型,并且使用Kriging函数值即使在响应不平滑的情况下也可以稳健地评估输出不确定性,同时使用Kriging预测变量的拟合不确定性和梯度信息进行动态自适应采样。与现有的多项式混沌扩展和仅基于Kriging预测因子拟合不确定性的自适应采样方法相比,基于Kriging模型的UQ方法在估计输出解决方案的非平滑响应方面,在准确性和鲁棒性方面表现出优异的性能。首先在统一不确定性下对分析的非光滑函数进行了测试,然后通过将拟议的UQ方法与CFD耦合,将其应用于自由流马赫数下具有正常不确定性的跨音速RAE 2822翼型流动。

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