A Multi-Fidelity Uncertainty Propagation Model for Multi-Dimensional Correlated Flow Field Responses

Jiangtao Chen, Jiao Zhao, Wei Xiao, Luogeng Lv, Wei Zhao, Xiaojun Wu
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Abstract

Given the randomness inherent in fluid dynamics problems and limitations in human cognition, Computational Fluid Dynamics (CFD) modeling and simulation are afflicted with non-negligible uncertainties, casting doubts on the credibility of CFD. Scientifically and rigorously quantifying the uncertainty of CFD is paramount for assessing its credibility and informing engineering decisions. In order to quantify the uncertainty of multidimensional flow field responses stemming from uncertain model parameters, this paper proposes a method based on Gappy Proper Orthogonal Decomposition (POD) for supplementing high-fidelity flow field data within a framework that leverages POD and surrogate models. This approach enables the generation of corresponding high-fidelity flow fields from low-fidelity ones, significantly reducing the cost of high-fidelity flow field computation in uncertainty propagation modeling. Through an analysis of the impact of uncertainty in the coefficients of the Spalart–Allmaras (SA) turbulence model on the distribution of wall friction coefficients for the NACA0012 airfoil and pressure coefficients for the M6 wing, the proposed multi-fidelity modeling approach is demonstrated to offer significant advancements in both accuracy and efficiency compared to single-fidelity methods, providing a robust and efficient prediction model for large-scale random sampling.
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多维相关流场响应的多保真度不确定性传播模型
鉴于流体动力学问题固有的随机性和人类认知的局限性,计算流体动力学(CFD)建模和仿真存在不可忽略的不确定性,这使人们对 CFD 的可信度产生怀疑。科学、严格地量化 CFD 的不确定性对于评估其可信度和为工程决策提供信息至关重要。为了量化不确定模型参数引起的多维流场响应的不确定性,本文提出了一种基于 Gappy 适当正交分解(POD)的方法,用于在利用 POD 和代用模型的框架内补充高保真流场数据。这种方法可以从低保真流场生成相应的高保真流场,大大降低了不确定性传播建模中高保真流场计算的成本。通过分析 Spalart-Allmaras(SA)湍流模型系数的不确定性对 NACA0012 翼面壁面摩擦系数和 M6 机翼压力系数分布的影响,证明了与单保真度方法相比,所提出的多保真度建模方法在精度和效率方面都有显著提高,为大规模随机采样提供了稳健高效的预测模型。
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