4.7 Article

Transition-based constrained large-eddy simulation method with application to an ultrahigh-lift low-pressure turbine cascade flow

期刊

JOURNAL OF FLUID MECHANICS
卷 941, 期 -, 页码 -

出版社

CAMBRIDGE UNIV PRESS
DOI: 10.1017/jfm.2022.286

关键词

turbulence modelling; turbulence simulation; turbulent transition

资金

  1. National Natural Science Foundation of China [92152202, 11988102]
  2. National Key Project [GJXM92579]

向作者/读者索取更多资源

This study introduces a transition-predictive Reynolds-averaged Navier-Stokes (RANS) model to improve the ability of constrained large-eddy simulation (TrCLES) in predicting wall-bounded laminar-turbulent transition flows. The TrCLES method is validated in simulations of external and internal flows, and compared with other existing methods. The results show that the TrCLES method accurately predicts laminar separation bubble and separation-induced transition process.
A transition-predictive Reynolds-averaged Navier-Stokes (RANS) model is introduced as the Reynolds controlling condition to constrained large-eddy simulation (TrCLES) to improve the ability of this method to predict wall-bounded laminar-turbulent transition flows. In the TrCLES method, the constraint conditions for total Reynolds stress and heat flux are only imposed to the near-wall region in transitional and turbulent boundary layer. The newly proposed method recovers direct numerical simulation in the laminar boundary region, and retrieves the traditional large-eddy simulation method in the far-wall regions. The TrCLES method is validated in simulations of external flow around the Eppler 387 (E387) airfoil and internal flow past the ultrahigh-lift low-pressure turbine T106C cascade. The improved delayed detached-eddy simulation (IDDES) method, CLES method based on full-turbulence shear stress transport model and RANS method with a three-equation transition model are also evaluated in comparison with the available experimental and numerical data. As expected, the TrCLES method can predict laminar separation bubble and separation-induced transition process in both the E387 and T106C flows pretty well. In contrast, neither IDDES nor the original CLES can provide reasonable prediction for the laminar separation-induced transition phenomenon. The validity and fidelity of the TrCLES method are further verified by simulations of the T106C cascade flows in a wider range of exit Reynolds and Mach numbers. It is shown that the TrCLES method can not only predict the time-averaged aerodynamic quantities such as isentropic Mach number and exit kinetic energy loss very well, but also capture the laminar separation bubble and unsteady flow structures with satisfactory accuracy.

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