Article ID Journal Published Year Pages File Type
5472637 Aerospace Science and Technology 2017 12 Pages PDF
Abstract
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.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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