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Establishment of a High Quality Database for the Modelling of Perforated Liners

[+] Author Affiliations
Claus Heuwinkel, Lars Enghardt, Friedrich Bake

German Aerospace Center (DLR), Berlin, Germany

Sermed Sadig, Miklós Gerendás

Rolls-Royce Deutschland Ltd. & Co. KG, Dahlewitz, Germany

Paper No. GT2010-22329, pp. 247-258; 12 pages
  • ASME Turbo Expo 2010: Power for Land, Sea, and Air
  • Volume 2: Combustion, Fuels and Emissions, Parts A and B
  • Glasgow, UK, June 14–18, 2010
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-4397-0 | eISBN: 978-0-7918-3872-3
  • Copyright © 2010 by ASME and Rolls-Royce Deutschland Ltd. & Co KG


Perforated liners, especially in combination with a bias flow, are very effective sound absorbers. Applied to gas turbine combustors they can suppress thermoacoustic instabilities and thus allow the application of new combustion concepts concerning higher efficiency and lower emissions. While the successful application of such a damping concept has been shown, it is still not possible to accurately predict the damping performance of a given configuration. This paper provides a comprehensive database of high quality experimental data. Variations of geometric, fluid mechanic and acoustic parameters have been studied, including realistic engine configurations. The results demonstrate each parameters influence on the damping performance. A low order thermo-acoustic model is used to simulate the test configurations numerically. The model shows a good agreement with the measurements for a wide range of geometries, Strouhal and bias flow Mach numbers.

Copyright © 2010 by ASME and Rolls-Royce Deutschland Ltd. & Co KG
Topics: Modeling , Databases



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