多维相关流场响应的不确定性量化

IF 0.5 Q4 ENGINEERING, MECHANICAL Journal of Verification, Validation and Uncertainty Quantification Pub Date : 2024-03-13 DOI:10.1115/1.4065070
Wei Zhao, Luogeng Lv, Jiao Zhao, Wei Xiao, Jiangtao Chen, Xiaojun Wu
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引用次数: 0

摘要

流体动力学问题固有的随机性或人类认知的局限性导致了 CFD 建模和仿真中不可忽略的不确定性,从而导致人们对 CFD 结果的可信度产生怀疑。因此,科学、严格地量化这些不确定性对于评估 CFD 预测的可靠性和做出明智的工程决策至关重要。虽然针对单个输出量已开发出成熟的不确定性传播方法,但多维相关流场变量的不确定性传播仍面临挑战。本文提出了一种基于适当正交分解和人工神经网络的先进不确定性传播建模方法。通过将多维相关响应投影到正交基函数空间,输出的维度大大降低,从而简化了后续的模型训练过程。建立的人工神经网络可将 CFD 模型的不确定参数映射到基函数系数。由于通过适当的正交分解实现了流场变量和基函数系数的双向表示,结合人工神经网络建模,实现了在任何模型参数下对流场变量的快速预测。为了有效识别影响最大的模型参数,我们采用了基于协方差分解的多输出全局灵敏度分析方法。通过 NACA0012 机翼和 M6 机翼这两个示例,我们证明了我们提出的方法在不同模型系数下预测多维流场变量的准确性和有效性。我们进行了大规模随机抽样,以量化不确定性,并找出对整个流场有重大影响的关键因素。
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Uncertainty Quantification for Multi-Dimensional Correlated Flow Field Responses
The inherent randomness of fluid dynamics problems or human cognitive limitations results in non-negligible uncertainties in CFD modeling and simulation, leading to doubts about the credibility of CFD results. Therefore, scientific and rigorous quantification of these uncertainties is crucial for assessing the reliability of CFD predictions and informed engineering decisions. Although mature uncertainty propagation methods have been developed for individual output quantities, the challenges lie in the multi-dimensional correlated flow field variables. This article proposes an advanced uncertainty propagation modeling approach based on proper orthogonal decomposition and artificial neural networks. By projecting the multi-dimensional correlated responses onto an orthogonal basis function space, the dimensionality of output is significantly reduced, simplifying the subsequent model training process. An artificial neural network that maps the uncertain parameters of the CFD model to the coefficients of the basis functions is established. Due to the bidirectional representation of flow field variables and basis function coefficients through proper orthogonal decomposition, combined with artificial neural network modeling, rapid prediction of flow field variables under any model parameters is achieved. To effectively identify the most influential model parameters, we employ a multi-output global sensitivity analysis method based on covariance decomposition. Through two exemplary cases of NACA0012 airfoil and M6 wing, we demonstrate the accuracy and efficacy of our proposed approach in predicting multi-dimensional flow field variables under varying model coefficients. Large-scale random sampling is conducted to quantify the uncertainties and identify the key factors that significantly impact the overall flow field.
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来源期刊
CiteScore
1.60
自引率
16.70%
发文量
12
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