Bayesian uncertainty analysis of SA turbulence model for supersonic jet interaction simulations

被引:28
作者
Li, Jinping [1 ]
Chen, Shusheng [2 ,3 ]
Cai, Fangjie [4 ]
Wang, Sheng [1 ]
Yan, Chao [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100083, Peoples R China
[2] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China
[3] AVIC First Aircraft Inst, Xian 710089, Peoples R China
[4] China Acad Launch Vehicle Technol, Beijing 100076, Peoples R China
基金
中国国家自然科学基金;
关键词
Bayesian calibration; MAP estimation; SA turbulence model; Supersonic jet interaction; Uncertainty quantification; EPSILON MODEL; SENSITIVITY; CALIBRATION; RANS; FLUX;
D O I
10.1016/j.cja.2021.07.039
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Reynolds Averaged Navier-Stokes (RANS) models are still the workhorse in current engineering applications due to its high efficiency and robustness. However, the closure coefficients of RANS turbulence models are determined by model builders according to some simple fundamental flows, and the suggested values may not be applicable to complex flows, especially supersonic jet interaction flow. In this work, the Bayesian method is employed to recalibrate the closure coefficients of Spalart-Allmaras (SA) turbulence model to improve its performance in supersonic jet interaction problem and quantify the uncertainty of wall pressure and separation length. The embedded model error approach is applied to the Bayesian uncertainty analysis. Firstly, the total Sobol index is calculated by non-intrusive polynomial chaos method to represent the sensitivity of wall pressure and separation length to model parameters. Then, the pressure data and the separation length are respectively served as calibration data to get the posterior uncertainty of model parameters and Quantities of Interests (QoIs). The results show that the relative error of the wall pressure predicted by the SA turbulence model can be reduced from 14.99% to 2.95% through effective Bayesian parameter estimation. Besides, the calibration effects of four likelihood functions are systematically evaluated. The posterior uncertainties of wall pressure and separation length estimated by different likelihood functions are significantly discrepant, and the Maximum a Posteriori (MAP) values of parameters inferred by all functions show better performance than the nominal values. Finally, the closure coefficients are also estimated at different jet total pressures. The similar posterior distributions of model parameters are obtained in different cases, and the MAP values of parameters calibrated in one case are also applicable to other cases. (C) 2021 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
引用
收藏
页码:185 / 201
页数:17
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