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Affordable Uncertainty Quantification for Industrial Problems: Application to Aero-Engine Fans

机译:工业问题的负担得起的不确定性量化:在航空发动机风扇中的应用

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摘要

Uncertainty quantification (UQ) is an increasingly important area of research. As components and systems become more efficient and optimized, the impact of uncertain parameters is likely to become critical. It is fundamental to consider the impact of these uncertainties as early as possible during the design process, with the aim of producing more robust designs (less sensitive to the presence of uncertainties). The cost of UQ with high-fidelity simulations becomes therefore of fundamental importance. This work makes use of least-squares approximations in the context of appropriately selected polynomial chaos (PC) bases. An efficient technique based on QR column pivoting has been employed to reduce the number of evaluations required to construct the approximation, demonstrating the superiority of the method with respect to full-tensor quadrature (FTQ) and sparse-grid quadrature (SGQ). Orthonormal polynomials used for the PC expansion are calculated numerically based on the given uncertainty distribution, making the approach optimal for any type of input uncertainty. The approach is used to quantify the variability in the performance of two large bypass-ratio jet engine fans in the presence of shape uncertainty due to possible manufacturing processes. The impacts of shape uncertainty on the two geometries are compared, and sensitivities to the location of the blade shape variability are extracted. The mechanisms at the origin of the change in performance are analyzed in detail, as well as the differences between the two configurations.
机译:不确定度量化(UQ)是一个日益重要的研究领域。随着组件和系统变得更加高效和优化,不确定参数的影响可能会变得至关重要。至关重要的是,在设计过程中尽早考虑这些不确定性的影响,目的是生成更可靠的设计(对不确定性的存在不那么敏感)。因此,采用高保真模拟的UQ成本变得至关重要。这项工作在适当选择的多项式混沌(PC)基的情况下使用了最小二乘近似。已采用基于QR列枢轴的有效技术来减少构造近似值所需的评估次数,这证明了该方法相对于全张量正交(FTQ)和稀疏网格正交(SGQ)的优越性。根据给定的不确定性分布,对用于PC扩展的正交多项式进行数值计算,从而使该方法对于任何类型的输入不确定性都是最佳的。该方法用于量化由于可能的制造工艺而导致形状不确定的情况下,两个大型旁路比率喷气发动机风扇的性能差异。比较了形状不确定性对两个几何形状的影响,并提取了对叶片形状可变性位置的敏感性。详细分析了性能变化产生的机理,以及两种配置之间的差异。

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  • 来源
    《Journal of turbomachinery 》 |2018年第6期| 061005.1-061005.12| 共12页
  • 作者单位

    Univ Cagliari, Dept Mech Chem & Mat Engn, I-09123 Cagliari, Italy;

    Aerothermal Design Syst Rolls Royce Plc, Derby DE24 8BJ, England;

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