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LES of the aero-acoustic coupling in acoustic liners containing multiple cavities

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Academic year: 2021

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Figure

Fig. 1 The single (left, a), and multiple (right, b) configurations investigated. For both cases, the tip boundary condition can be switched from anechoic to reflecting.
Table 1 Configurations investigated in this paper, where N c is the number cavities and N cells the number of
Fig. 3 Instantaneous snapshot (middle) of the Q-criterion for case C101_3D_S, highlighted by zooms (bottom) to indicate the evolution of the 3D boundary layer along the liner
Fig. 4 Instantaneous snapshot (middle) of the z-component of the 2D vorticity field for case C101_2D_U, highlighted by zooms (bottom) to indicate the evolution of the 2D boundary layer along the liner
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