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Experimental Validation of Polynomial Chaos Theory on an Aircraft T-Tail

机译:飞机尾翼多项式混沌理论的实验验证

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Uncertainty quantification (UQ) is a notion which has received much interest over the past decade. It involves the extraction of statistical information from a problem with inherent variability, where this variability may stem from a lack of model knowledge or through observational uncertainty. Traditionally, UQ has been a challenging pursuit owing to the lack of efficient methods available. The archetypal UQ method is Monte Carlo theory, however this method possesses a slow convergence rate and is therefore a computational burden. In contrast to Monte Carlo theory, polynomial chaos theory aims to spectrally expand the modelled uncertainty via polynomials of random variables which have deterministic coefficients. Once the spectral expansion has been fully defined, it is possible to obtain statistical properties using simple integration procedures. Although literature has proven polynomial chaos theory to be more efficient than Monte Carlo theory in several contexts, there has been very little effort to experimentally validate polynomial chaos theory. Hence, it is the aim of this paper to perform an experimental validation on an in-house physical T-Tail structure by analysing the first six vibrational modes of this structure, and comparing these against the predicted uncertainty bounds of polynomial chaos theory.
机译:不确定性量化(UQ)是一个概念,在过去十年中引起了人们的极大兴趣。它涉及从具有固有变异性的问题中提取统计信息,其中,这种变异性可能是由于缺乏模型知识或观测不确定性引起的。传统上,由于缺乏可用的有效方法,UQ一直是具有挑战性的追求。原型UQ方法是蒙特卡洛理论,但是该方法收敛速度较慢,因此是计算负担。与蒙特卡洛理论相反,多项式混沌理论旨在通过具有确定性系数的随机变量多项式在光谱上扩展建模的不确定性。一旦完全定义了光谱扩展,就可以使用简单的积分程序获得统计特性。尽管文献已证明多项式混沌理论在某些情况下比蒙特卡洛理论更有效,但很少有人通过实验来验证多项式混沌理论。因此,本文的目的是通过分析该结构的前六个振动模式,并将其与多项式混沌理论的预测不确定性范围进行比较,对内部物理T尾结构进行实验验证。

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