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Uncertainty and sensitivity analysis of flow parameters for transition models on hypersonic flows

机译:高超声速流过渡模型流动参数的不确定性和敏感性分析

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The impossibility to reproduce the experimental conditions, which is difficult to perfectly control and inevitably fluctuate, raises the uncertainties in numerical simulation. The objective of this work is to quantify the uncertainty and sensitivity of hypersonic transition modeling due to uncertainty in the flow parameters. Two representative transition models, e.g. gamma-Re-theta and k-omega-gamma, are considered. And five flow parameters including freesteam Mach number, pressure, temperature, turbulence intensity and wall temperature are selected as aleatory uncertain variables uniformly distributing among the bound. Then the stochastic expansions based on point-collocation non-intrusive polynomial chaos (NIPC) method is utilized to represent and propagate the uncertainties in the output quantities of interests (Qols) for hypersonic flow over the flat plate and the straight cone. Benefiting from the efficiency of the NIPC method, accurate uncertainty results are obtained with only 42 evaluations for each problem. Furthermore, Sobol indices are utilized to provide a relative ranking of each input uncertainty to the overall uncertainty in the output. The uncertainty results quantitatively verify that the transition zone is great sensitive to changes in flow parameters. Besides, for both the heat flux and skin friction coefficient, the importance ranking of the flow parameters and their trends are roughly resemble between the gamma-Re-theta and k-omega-gamma model. This signifies that their sensitivity with respect to the input parameters is mainly associated with flow features rather than transition models. However, the contrary is the case for uncertainty in transition onset and length whose sensitivity to uncertainties of input parameters depends strongly on transition models. The present investigation shows that the freestream pressure is the greatest contributor to uncertainty in most cases. The freestream turbulence intensity, whose effect can be nearly negligible in heat flux and C-f, plays a predominant role on transition length. (C) 2019 Elsevier Ltd. All rights reserved.
机译:无法再现实验条件,难以完美控制且不可避免地波动,这增加了数值模拟的不确定性。这项工作的目的是量化由于流动参数的不确定性而导致的超音速过渡模型的不确定性和敏感性。两个代表性的过渡模型,例如考虑了γ-Re-θ和k-ω-γ。选择了自由蒸汽马赫数,压力,温度,湍流强度和壁温等五个流动参数作为均匀分布在边界之间的不确定不确定变量。然后,利用基于点配置非侵入式多项式混沌(NIPC)方法的随机展开来表示和传播平板和直锥上高超声速流动的目标输出量(Qols)的不确定性。得益于NIPC方法的效率,每个问题仅需进行42次评估即可获得准确的不确定性结果。此外,Sobol指数用于提供每个输入不确定性与输出中总体不确定性的相对排名。不确定性结果定量验证了过渡带对流量参数的变化非常敏感。此外,对于热通量和皮肤摩擦系数而言,流动参数的重要性等级及其趋势大致类似于γ-Re-theta模型和k-ω-γ模型。这表明它们对输入参数的敏感性主要与流量特征相关,而不与过渡模型相关。但是,对于过渡开始和长度的不确定性则相反,其对输入参数不确定性的敏感性在很大程度上取决于过渡模型。目前的研究表明,在大多数情况下,自由流压力是导致不确定性的最大因素。自由流湍流强度在过渡长度上起主要作用,其湍流强度在热通量和C-f中几乎可以忽略不计。 (C)2019 Elsevier Ltd.保留所有权利。

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