航空学报 > 2024, Vol. 45 Issue (S1): 730574-730574   doi: 10.7527/S1000-6893.2024.30574

两种SST湍流模型改进方法适用性分析

曾宇, 汪洪波(), 连城阅, 杨揖心, 熊大鹏, 孙明波, 刘卫东   

  1. 国防科技大学 空天科学学院 高超声速技术实验室,长沙 410073
  • 收稿日期:2024-04-23 修回日期:2024-04-25 接受日期:2024-04-30 出版日期:2024-12-25 发布日期:2024-05-08
  • 通讯作者: 汪洪波 E-mail:whbwatch@nudt.edu.cn
  • 基金资助:
    国家自然科学基金(12102471)

Applicability analysis of two improved methods of SST turbulence model

Yu ZENG, Hongbo WANG(), Chengyue LIAN, Yixin YANG, Dapeng XIONG, Mingbo SUN, Weidong LIU   

  1. Hypersonic Technology Laboratory,College of Aerospace Science,National University of Defense Technology,Changsha 410073,China
  • Received:2024-04-23 Revised:2024-04-25 Accepted:2024-04-30 Online:2024-12-25 Published:2024-05-08
  • Contact: Hongbo WANG E-mail:whbwatch@nudt.edu.cn
  • Supported by:
    National Natural Science Foundation of China(12102471)

摘要:

雷诺平均湍流模型计算效率高,在工程应用上具有重要意义。传统模式与新型数据驱动模式湍流模型改进旨在提升湍流模型预测精度。然而,新型数据驱动模式大多针对低速流动,对其在高速流动中的应用、评估以及推广较少。两种模式对比性研究的缺乏也给二者的合理利用产生了困扰。在标准雷诺剪切应力输运(SST)模型框架下,一方面采用传统模式引入可压缩效应作用于输运方程耗散项,另一方面根据新型数据驱动模式引入耗散项修正。两种模式下的改进主要作用于流场中的剪切层。超声速压缩拐角和超声速凹腔斜坡算例的测试结果表明,新型数据驱动模式可以获得不同物理特征量之间初步的、可解释的非线性关系,但需经过传统模式的调整与再优化才能应用,具有一定的推广性,在捕捉某些湍流细节方面表现出优于传统模式的性能,但精度仍有待提高。

关键词: 湍流模型, SST, 数据驱动技术, 可压缩, 分离流, 符号回归

Abstract:

The Reynolds-averaged turbulence model has high computational efficiency, and is of great significance in engineering applications. The purpose of the improvement of the traditional and the new data-driven modes of turbulence model is to improve the prediction accuracy. However, the new data-driven mode is mainly for the low-speed flow, and there are less reports on the application, evaluation and promotion of the mode for the high-speed flow. The lack of comparative study of the two modes also causes problems for their rational use. Under the frame of the standard Reynolds Shear Stress Transport (SST) model, the traditional mode is adopted to introduce the compressibility effect into the dissipative term of the transport equation, and the new data-driven mode is used to modify the dissipative term. The improvement in the two modes mainly acts on the shear layer in the flow field. The test results of supersonic compression corner and supersonic cavity ramp show that the new data-driven mode can obtain a preliminary and explainable nonlinear relationship between different physical characteristics, but can only be applied after adjustment and re-optimization of the traditional mode. It has a certain generalization and is better than the traditional mode in capturing some turbulence details, but the accuracy still needs to be improved.

Key words: turbulence model, SST, data-driven technology, compressible, separated flow, symbolic regression

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