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Exploring Stochastic Models for Fast Analysis of Unsteady Wing Aerodynamics

机译:快速分析不稳定翼空气动力学的随机模型

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Wings, hydrofoils, and other lifting surfaces often operate in highly unsteady inflow conditions, such as gusty wind or waves. These inflows are unsteady on many time scales and have to be considered a stochastic process. For fluid dynamics practitioners, this leads to a challenge: how can the long term, random design loads (e.g. fatigue or 20-year return extreme) be quantified efficiently? The conventional approach to this challenge involves analysis of a large set of short term inflow realizations and extrapolates the results to long term loads via their assumed probability distributions. However, this requires solving many simulations separately. This is computationally expensive and presents a handicap, especially in early design stages (optimization), where rapid evaluations of candidate designs and their gradients with respect to design variables are required. To tackle this problem, we introduce two alternative stochastic methods, one based on a Galerkin projection onto a set of Fourier modes, and the other based on a Polynomial Chaos Expansion. These stochastic approaches enables us to carry the randomness though the solution process to directly obtain a stochastic result. Thus long term loads can be directly constructed from the stochastic solution, without having to analyze specific realizations of the inflow inputs. The new processes are illustrated and discussed with an example based on a rectangular wing lifting line model.
机译:翅膀,水翼和其他升降表面经常在高度不稳定的流入条件下操作,例如胃肠风或波浪。这些流入在许多时间尺度上是不稳定的,并且必须被认为是随机过程。对于流体动态从业者,这导致挑战:如何有效地量化长期,随机设计负荷(例如疲劳或20年回报极端)?这种挑战的传统方法涉及分析大量的短期流入实现,并通过假设的概率分布将结果推断到长期负载。但是,这需要单独解决许多模拟。这是计算昂贵的并且呈现一个障碍,尤其是在早期设计阶段(优化),其中需要候选设计的快速评估及其相对于设计变量的梯度。为了解决这个问题,我们介绍了两种替代随机方法,一个基于Galerkin投影到一组傅里叶模式,另一个基于多项式混沌扩展。这些随机方法使我们能够携带随机性,尽管解决方案过程直接获得随机结果。因此,可以从随机解决方案直接构建长期载荷,而无需分析流入输入的特定实现。示出并用基于矩形翼升降线模型的示例进行了讨论的新过程。

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