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Computational Modelling of Flow and Scalar Transport Accounting for Near-Wall Turbulence with Relevance to Gas Turbine Combustors

  • S. JakirlićEmail author
  • R. Jester-Zürker
  • G. John-Puthenveettil
  • B. Kniesner
  • C. Tropea
Chapter
Part of the Fluid Mechanics and Its Applications book series (FMIA, volume 1581)

Abstract

An overview is given of the activities in the framework of the German Collaborative Research Center “Flow and Combustion in Future Gas Turbine Combustion Chambers” (Sonderforschungsbereich SFB 568) concerning the development of computational models in the framework of the conventional RANS method with special focus on the near-wall turbulence and a method combining a near-wall RANS models in the wall vicinity with the conventional LES in the core flow and their applications to the flow separating from sharp-edged and continuous surfaces and different swirl combustor configurations under the conditions of constant and variable fluid properties.

Keywords

RANS Hybrid LES/RANS Reynolds stress and scalar-flux transport models Near-wall turbulence Flow separation Swirling flows Variable fluid properties 

Notes

Acknowledgements

The authors acknowledge the financial support from the German Research Council (DFG) through the SFB568.

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Copyright information

© Springer Science+Business Media Dordrecht 2013

Authors and Affiliations

  • S. Jakirlić
    • 1
    • 2
    Email author
  • R. Jester-Zürker
    • 1
    • 3
  • G. John-Puthenveettil
    • 1
  • B. Kniesner
    • 1
    • 4
  • C. Tropea
    • 1
    • 2
  1. 1.Department of Mechanical Engineering, Institute of Fluid Mechanics and AerodynamicsTechnische Universität DarmstadtDarmstadtGermany
  2. 2.Center of Smart InterfacesTechnische Universität DarmstadtDarmstadtGermany
  3. 3.Voith Hydro Holding GmbH & CoHeidenheimGermany
  4. 4.TP24 System AnalysisAstrium Space TransportationMunichGermany

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