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Computational study of aero-acoustic sources in perforate silencers
Reynolds Averaged Navier Stokes and Large Eddy Simulations of two perforate plates at a overall pressure ratio of 1.45 have been performed to allow analysis of the sensitivity of acoustic noise sources to porosity. Two geometries are presented: A 23% porosity and a 40% porosity 1mm plate with 2mm di...
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| Main Authors: | , |
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| Format: | Default Conference proceeding |
| Published: |
2011
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/9542 |
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