摘要
With the explosive development of the Computational Fluid Dynamics (CFD), many researchers studied accurate Reynolds Averaged Navier–Stokes (RANS) simulations in low-speed flows by analyzing turbulence modeling or high order reconstruction methods. Few people noticed the influence of the accuracy of spatial scheme for low-speed flow on the RANS simulations. In this paper, we conduct a systematic study on this issue. After a verification of our compressible code, the following four numerical tests are conducted: the flat plate, the NACA0012 airfoil, the NACA4412 airfoil, and the backward facing step. Grid convergent results in these cases show that a high level of accuracy at low speeds is beneficial to the steady RANS computations.
源语言 | 英语 |
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页(从-至) | 578-589 |
页数 | 12 |
期刊 | Aerospace Science and Technology |
卷 | 70 |
DOI | |
出版状态 | 已出版 - 11月 2017 |
已对外发布 | 是 |