《表2 网格分布：雷诺数对机翼尾缘噪声的影响（英文）》

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《雷诺数对机翼尾缘噪声的影响（英文）》

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The time step non-dimensonalized by the chord length and the freestream velocity is 4×10-5，with the maximum CFL number less than unit.The total time steps calculated are 6×105，corresponding to a time duration that the freestream flow pass a distance of 24chord length.After the computation of the first 2×105 time steps，flow reaches a quasisteady state，then instantaneous flow fields of the remaining 4×105 time steps are collected for obtaining time-averaged and statistical data for subsequent analysis.