A Methodology for On the Fly Acoustic Characterization of the Feeding Line Impedances in a Turbulent Swirled Combustor

A methodology is proposed to determine on the fly the acoustic impedances at the boundaries of a combustor under operation and without the need for an external forcing device. The methodology is applied hereby to obtain the reflection coefficients of the air and fuel feeding lines supplying a swirle...

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Veröffentlicht in:Journal of engineering for gas turbines and power 2011-01, Vol.133 (1)
Hauptverfasser: Lamraoui, A, Richecoeur, F, Schuller, T, Ducruix, S
Format: Artikel
Sprache:eng
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