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Reduced Basis Isogeometric Methods (RB-IGA) for the real-time simulation of flows about parametrized NACA airfoils

机译:用于参数化NACA机翼气流实时模拟的简化基本等距方法(RB-IGA)

摘要

We present a Reduced Basis (RB) method based on Isogeometric Analysis (IGA) for the rapid and reliable evaluation of PDE systems characterized by complex geometrical features. At the current state of the art, this is the first case of coupling between RB and IGA methods. The construction of the RB method relies on an Isogeometric Boundary Element Method (IGA-BEM) as the high-fidelity technique, allowing a direct interface with Computer Aided Design (CAD) tools. A suitable Empirical Interpolation Method (EIM) ensures an efficient offline/online decomposition between the construction and the evaluation of the RB method. We consider the real-time simulation of potential flows past airfoils, parametrized with respect to the angle of attack and the NACA number identifying their shape, and we provide a validation of our methodology with respect to experimental data and reference numerical codes, showing in both cases a very good agreement.
机译:我们提出基于等几何分析(IGA)的简化基础(RB)方法,以快速,可靠地评估以复杂几何特征为特征的PDE系统。在当前的现有技术中,这是RB和IGA方法之间耦合的第一种情况。 RB方法的构建依赖于等高边界元素方法(IGA-BEM)作为高保真技术,从而可以与计算机辅助设计(CAD)工具直接交互。合适的经验插值方法(EIM)可确保在RB方法的构造和评估之间进行有效的脱机/在线分解。我们考虑了通过机翼的潜在流动的实时模拟,并根据攻角和确定其形状的NACA数进行了参数化,并针对实验数据和参考数字代码对方法进行了验证,两者均显示案件达成了很好的协议。

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