Response surface method optimization of uniform and axially segmented duct acoustic liners
An extensive duct acoustics propagation study is presented that has been conducted to assess the design of a liner for an aeroengine inlet duct. The aim is to predict how different liner configurations, at various flight conditions affect the attenuation of sound in an inlet. Two different noise sou...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
2006.
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| Subjects: | |
| Online Access: | Get fulltext |