4.7 Article

Numerical investigation of corner separation flow using Spalart-Allmaras model with various modifications

期刊

AEROSPACE SCIENCE AND TECHNOLOGY
卷 127, 期 -, 页码 -

出版社

ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2022.107682

关键词

Corner separation; Transonic compressor rotor; Turbulent non-equilibrium transport characteristics; Anisotropy; Nonlinear constitutive relation

资金

  1. National Natural Science Foundation of China [51976006, 51790513]
  2. Aeronautical Science Foundation of China [2018ZB51013]
  3. National Science and Tech-nology Major Project [2017-II-003-0015]
  4. High-Performance Computing Centre of Beihang University

向作者/读者索取更多资源

This study conducts numerical simulations of corner separation flow and compares the predictive capabilities of various turbulence models. The results show that, with the modifications considering turbulent non-equilibrium transport characteristics and turbulence anisotropy, the SA-Helicity and SA-Helicity-QCR2013 models have more accurate predictions.
Three-dimensional corner separation is an inherent flow feature in axial compressors which blocks flow path and worsens the performance. To find an effective turbulence model for such flow, numerical simulations of the corner separation flow are conducted in the prescribed velocity distribution (PVD) cascade using the Spalart-Allmaras (SA) model with various modifications. Turbulence models studied here include the SA model, the SA-neg model, the SA-noft2 model, the SA-R model, the SA-RC model, the SA-Helicity model, the SA-KL model, the SA-S model and their combinations with the quadratic constitutive relation (QCR) corrections. Compared with the experiment, the SA-Helicity model predicts more accurately than SA model with other commonly used modifications which indicates the importance of reasonably considering turbulent non-equilibrium transport characteristics in large-scale vortices. With the QCR corrections for considering turbulence anisotropy, the blending models perform better than the original SA model but most of them still overpredict the separation region. Among them, the SA-HelicityQCR2013 model which provides a similar result as the SA-Helicity model performs the best. In further validations based on the transonic compressor NASA Rotor 67, the SA-Helicity and SA-Helicity-QCR2013 models can still give more accurate predictions, which is reflected in the stall margin as well as the spanwise distributions of total pressure and total temperature at both the near peak efficiency and the near stall conditions. The universality of the helicity correction is proved to a certain extent. In future turbulence modeling studies of turbomachinery internal flows, it is necessary to reasonably consider turbulence non-equilibrium and turbulence anisotropy in large-scale vortices. (C) 2022 Elsevier Masson SAS. All rights reserved.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据