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Direct Aeroacoustic Simulation with Volume Penalization Method

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Figure

Figure 1. Configurations of flow around a cascade of flat plates and that around a circular cylinder
Table 1. Computational parameters.
Figure 2 shows the distributions of the time-averaged pressure coefficient predicted by the present computational method compared with those by Inoue and Hatakeyama [5]
Figure 4. Comparison with experimental data. (a) Profiles of mean velocity, uh along x/b = 2.5

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