Acoustic and hydrodynamic analysis of the flow around an aerofoil with trailing-edge serrations
Direct numerical simulations of the flow around a NACA-0012 aerofoil are conducted, employing an immersed boundary method to represent flat-plate trailing-edge extensions both with and without serrations. Properties of the turbulent boundary layer convecting over the trailing edge are similar for bo...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
2012-09.
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| Subjects: | |
| Online Access: | Get fulltext |