基于贝叶斯估计的Navier-Stokes/DSMC耦合算法信息交换技术研究

Bayesian estimation-based information exchange techniques for coupled Navier-Stokes equation and DSMC algorithms

  • 摘要: 在Navier-Stokes(N-S)/直接模拟蒙特卡罗(direct simulation Monte Carlo, DSMC)耦合算法计算过程中,DSMC方法统计样本少,导致其计算结果存在很大的统计波动,这会对N-S方程的求解产生不利影响。为解决这一问题,本文在双向信息交换过程中引入用贝叶斯估计方法,并借用共轭先验分布理论,初步建立了一套基于贝叶斯估计的N-S/DSMC耦合信息交换框架。具体地,对密度、速度、移动温度采用正态分布的共轭先验分布函数;而对转动温度、振动温度,则采用伽玛分布的共轭先验分布函数。该方法将N-S方程上一步的计算结果作为先验信息,结合DSMC方法提供的统计样本,得到各参数的后验分布,并以其贝叶斯估计结果作为DSMC的计算结果,实现与N-S方程的信息交换。为验证该方法的有效性,分别对圆柱高速热化学非平衡流动和某飞行器过渡流区高速流动试验状态开展数值模拟。结果表明,在方差很大的情况下,合理选取超参数,基于贝叶斯估计和基于传统的“亚松弛”信息交换技术的计算结果温和良好,气动特性计算结果的最大误差为3.2%,而相较于风洞试验结果,最大误差在5%左右。上述结果验证了本文贝叶斯方法在抑制小样本统计波动方面的有效性。

     

    Abstract: In the calculation process of coupled Navier-Stokes (N-S) equation and direct simulation Monte Carlo (DSMC) algorithms, the DSMC method suffers from a limited number of statistical samples. This leads to significant statistical fluctuations in its results, which adversely affect the solution of the N-S equations. To address this issue, a Bayesian estimation approach is introduced into the two-way information exchange process. By leveraging the theory of conjugate prior distributions, a preliminary Bayesian estimation-based information exchange framework for N-S/DSMC coupling is established. Specifically, conjugate prior distributions of the normal type are adopted for density, velocity, and translational temperature. For rotational and vibrational temperatures, conjugate priors of the gamma type are employed. In this method, the computational results obtained from the N-S solver at the previous step are taken as prior information. These priors are then combined with the statistical samples provided by the DSMC method to yield the posterior distributions of the various flow parameters. The Bayesian estimates of these parameters are subsequently used as the DSMC results for information exchange with the N-S solver. To validate the proposed method, numerical simulations are performed for two test cases: a hypersonic thermochemical nonequilibrium flow over a cylinder, and a high-speed flow in the transitional regime over a flight vehicle under experimental conditions. The results demonstrate that, even in the presence of large variances, with appropriately selected hyperparameters, the proposed Bayesian approach yields results that agree well with those obtained using the conventional under-relaxation information exchange technique. The maximum discrepancy in predicted aerodynamic characteristics between the two methods is 3.2%. When compared against wind tunnel experimental data, the maximum error is approximately 5%. These findings confirm the effectiveness of the Bayesian method in suppressing statistical fluctuations caused by small sample sizes in DSMC computations.

     

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