Supplementary material to the publication 'Reynolds number effects in shock-wave/turbulent boundary-layer interactions'.

The supplementary material to the publication 'Reynolds number effects in shock-wave/turbulent boundary-layer interactions' involves animations of selected dynamic modes that should be considered in conjunction with the discussion. The selected modes include:A representative low-frequency mode from the SPDMD solution of each case (corresponding to figures 24 and 25 in the manuscript, which only show data for cases B1 and B3). The animations include the three-dimensional pressure, streamwise velocity and streamwise vorticity fields, and the corresponding modal frequencies are St_Lsep = 0.076 for the low-Reynolds case B1, St_Lsep =0.047 for the moderate-Reynolds case B2, and St_Lsep =0.039 for the high-Reynolds case B3.A representative mode with oscillation frequency around St_Lsep approx. 0.1 from the SPDMD solution of each case (corresponding to figure 29 in the manuscript, which only shows data for case B3). The animations also include the three-dimensional pressure, streamwise velocity and streamwise vorticity fields.The spanwise-averaged modal pressure from the selected dynamic mode of case B3 associated with St_Lsep approx. 0.1 (corresponding to figure 30 in the manuscript). The animation also includes the reconstructed separation line which is shown in black.The three-dimensional modal pressure of a representative high-frequency mode in the SPDMD solution of case B3 (St_Lsep = 0.375).论文《激波与湍流边界层相互作用中的雷诺数(Reynolds number)效应》的补充材料包含需配合正文讨论一同参考的选定动态模态动画。所选定的动态模态如下：各算例SPDMD求解所得的典型低频模态对应的动画（对应手稿中的图24与图25，仅展示了B1、B3算例的数据），该动画包含三维压力场、流向速度场与流向涡量场，对应的模态频率为：低雷诺数算例B1的St_Lsep=0.076，中等雷诺数算例B2的St_Lsep=0.047，高雷诺数算例B3的St_Lsep=0.039。各算例SPDMD求解所得的典型振荡频率约为St_Lsep≈0.1的模态对应的动画（对应手稿中的图29，仅展示了B3算例的数据），该动画同样包含三维压力场、流向速度场与流向涡量场。与B3算例St_Lsep≈0.1对应的选定动态模态的展向平均模态压力场动画（对应手稿中的图30），该动画同时包含以黑色绘制的重构分离线。B3算例SPDMD求解所得的典型高频模态的三维模态压力场动画（St_Lsep=0.375）。