Predicting turbulent flow over a backward-facing step using grid-adaptive simulation method
• Evaluation of hybrid RANS-LES methods is conducted on the flow over a backward-facing step using a coarser grid. • Sensitivity studies are made for numerical discretization , spanwise extent, and grid resolution for the GAS-SST method. • DMD analysis is conducted to validate the unsteady flow characteristics prediction of the GAS-SST method. Flow separation in backward-facing step (BFS) is a common phenomenon in engineering. The large scale of turbulent separation and reattachment makes it a challenge for the accurate prediction of such kinds of flows. Traditional hybrid Reynolds averaged Navier-Stokes (RANS) and large eddy simulation (LES) methods require relatively high grid resolutions, while the grid-adaptive simulation (GAS) method, a recently proposed hybrid RANS-LES method, can obtain high accuracy with reduced grid-resolution requirements. In this study, sensitivity studies of spanwise extent and grid resolution are conducted on the GAS method with the shear-stress transport (SST) k-ω turbulence model in simulating the BFS flow. Then, the delayed detached eddy simulation (DDES), improved DDES (IDDES), and scale-adaptive simulation (SAS), based on the SST model are compared with the GAS method for predicting the BFS flow with relatively low resolution of grid. The skin-friction and wall pressure coefficients, the velocity, and the resolved turbulent stress profiles predicted from different hybrid RANS-LES methods are compared with the experimental results. Results indicate that the GAS method can significantly outperform other hybrid RANS-LES methods when using coarser grid. The dynamic mode decomposition (DMD) analysis is conducted based on the GAS-SST results. Results show that GAS-SST with a low-resolution grid of 0.3 million cells can accurately predict key parameters such as mode shape, mode frequencies, spectral characteristics, and energy distribution of the main unsteady structures. Hence, a large amount of computational cost can be saved by the GAS method in comparison to the previous high-fidelity IDDES-SST simulation with a high-resolution grid of 14 million cells.
Authors
- Yangwei Liu (ORCID: https://orcid.org/0000-0001-9653-5760)
- Xindi Wei (ORCID: https://orcid.org/0000-0002-0313-339X)
- Yumeng Tang (ORCID: https://orcid.org/0000-0002-2131-3810)
- Guangyu Wang (ORCID: https://orcid.org/0000-0002-6798-9250)
Institutions
- Beihang University (CN)
Publication Details
- Journal
- Aerospace Science and Technology
- Published
- 2024-12-30
- DOI
- https://doi.org/10.1016/j.ast.2024.109913
- Citations
- 14
- Primary Topic
- Fluid Dynamics and Turbulent Flows
- Type
- article
- Field-Weighted Citation Impact
- 5.25