Volume 2: Combustion, Fuels and Emissions, Parts a and B 2011
DOI: 10.1115/gt2011-46303
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Assessment of Numerical Tools for the Evaluation of the Acoustic Impedance of Multi-Perforated Plates

Abstract: Multi-perforated liners, commonly employed in Gas Turbine combustors as cooling devices to control metal temperature, are recognized as very effective sound absorbers. Thus, in the innovative lean combustion technology, where the onset of thermoacoustic instabilities represents one of the most important issue, the multi-perforated plates can be exploited both for wall cooling and damping combustion instabilities.1

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Cited by 9 publications
(12 citation statements)
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“…The inlet patch is instead placed closer to the wall and the bias flow is generated by a totally reflecting velocity inlet. Such a scheme is equivalent to that exploited by Mendez and Eldredge [5] and Andreini et al [6].…”
Section: Normal Wavementioning
confidence: 92%
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“…The inlet patch is instead placed closer to the wall and the bias flow is generated by a totally reflecting velocity inlet. Such a scheme is equivalent to that exploited by Mendez and Eldredge [5] and Andreini et al [6].…”
Section: Normal Wavementioning
confidence: 92%
“…The proposed LES methodology is compared to a simplified approach which solve only for the acoustic field inside the liner and model the acoustic impedance of perforated plates with bias flow as an equivalent wall compliance, already presented in [6] and here briefly summarized.…”
Section: Howe Modelmentioning
confidence: 99%
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