Critical Sample-Size Analysis for Uncertainty Aerodynamic Evaluation of Compressor Blades with Stagger-Angle Errors

IF 2.1 3区 工程技术 Q2 ENGINEERING, AEROSPACE Aerospace Pub Date : 2023-11-25 DOI:10.3390/aerospace10120990
Haohao Wang, Limin Gao, Baohai Wu
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Abstract

Many probability-based uncertainty quantification (UQ) schemes require a large amount of sampled data to build credible probability density function (PDF) models for uncertain parameters. Unfortunately, the amounts of data collected as to compressor blades of aero-engines are mostly limited due to the expensive and time-consuming tests. In this paper, we develop a preconditioner-based data-driven polynomial chaos (PDDPC) method that can efficiently deal with uncertainty propagation of limited amounts of sampled data. The calculation accuracy of a PDDPC method is closely related to the sample size of collected data. Therefore, the influence of sample size on this PDDPC method is investigated using a nonlinear test function. Subsequently, we consider the real manufacturing errors in stagger angles for compressor blades. Under three different operating conditions, the PDDPC method is applied to investigate the effect of stagger-angle error on UQ results of multiple aerodynamic parameters of a two-dimensional compressor blade. The results show that as the sample-size of measured data increases, UQ results regarding aerodynamic performance obtained by the PDDPC method gradually converge. There exists a critical sample size that ensures accurate UQ analysis of compressor blades. The probability information contained in the machining error data is analyzed through Kullback–Leibler divergence, and the critical sample size is determined. The research results can serve as a valuable reference for the fast and cheap UQ analysis of compressor blades in practical engineering.
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对具有错开角度误差的压缩机叶片进行不确定性空气动力学评估的临界样本大小分析
许多基于概率的不确定性量化(UQ)方案需要大量的采样数据,才能为不确定参数建立可信的概率密度函数(PDF)模型。遗憾的是,由于测试昂贵且耗时,收集到的航空发动机压气机叶片数据量大多有限。在本文中,我们开发了一种基于前置条件器的数据驱动多项式混沌(PDDPC)方法,它能有效地处理有限采样数据的不确定性传播。PDDPC 方法的计算精度与采集数据的样本量密切相关。因此,我们使用非线性测试函数研究了样本量对 PDDPC 方法的影响。随后,我们考虑了压缩机叶片错开角的实际制造误差。在三种不同的运行条件下,应用 PDDPC 方法研究了交错角误差对二维压缩机叶片多个气动参数 UQ 结果的影响。结果表明,随着测量数据样本量的增加,PDDPC 方法获得的有关空气动力性能的 UQ 结果逐渐收敛。存在一个临界样本量,可以确保对压缩机叶片进行精确的 UQ 分析。通过 Kullback-Leibler 发散分析了加工误差数据中包含的概率信息,并确定了临界样本量。该研究成果可为实际工程中对压缩机叶片进行快速、廉价的 UQ 分析提供有价值的参考。
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来源期刊
Aerospace
Aerospace ENGINEERING, AEROSPACE-
CiteScore
3.40
自引率
23.10%
发文量
661
审稿时长
6 weeks
期刊介绍: Aerospace is a multidisciplinary science inviting submissions on, but not limited to, the following subject areas: aerodynamics computational fluid dynamics fluid-structure interaction flight mechanics plasmas research instrumentation test facilities environment material science structural analysis thermophysics and heat transfer thermal-structure interaction aeroacoustics optics electromagnetism and radar propulsion power generation and conversion fuels and propellants combustion multidisciplinary design optimization software engineering data analysis signal and image processing artificial intelligence aerospace vehicles'' operation, control and maintenance risk and reliability human factors human-automation interaction airline operations and management air traffic management airport design meteorology space exploration multi-physics interaction.
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