Abstract

Based on the detailed measurements of the unsteady boundary layer on the flat plate, which are affected by wakes generated from the moving circular cylinders, time-averaged characteristics of the boundary layer are calculated. Such characteristics are examined from viewpoint of the process of unsteady transition of the boundary layer. Furthermore, as for the time-averaged energy dissipation thickness of the boundary layer, some consideration is made to clarify the relation between the incident wakes and undesirable increase in total pressure loss, which is one of the important factors for aerodynamic designers of turbomachines.

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