A DRD finite element formulation for computing turbulent reacting flows in gas turbine combustors

A. Corsini, C. Iossa, F. Rispoli, Tayfun E. Tezduyar

研究成果: Article

46 引用 (Scopus)

抄録

An effective multiscale treatment of turbulent reacting flows is presented with the use of a stabilized finite element formulation. The method proposed is developed based on the streamline-upwind/Petrov-Galerkin (SUPG) formulation, and includes discontinuity capturing in the form of a new generation "DRD" method, namely the "DRDJ" technique. The stabilized formulation is applied to finite-rate chemistry modelling based on mixture-fraction approaches with the so-called presumed-PDF technique. The turbulent combustion process is simulated for an aero-engine combustor configuration of RQL concept in non-premixed flame regime. The comparative analysis of the temperature and velocity fields demonstrate that the proposed SUPG+DRDJ formulation outperforms the stand-alone SUPG method. The improved accuracy is demonstrated in terms of the combustor overall performance, and the mechanisms involved in the distribution of the numerical diffusivity are also discussed.

元の言語English
ページ(範囲)159-167
ページ数9
ジャーナルComputational Mechanics
46
発行部数1
DOI
出版物ステータスPublished - 2010 6
外部発表Yes

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Reacting Flow
Gas Turbine
Combustors
Turbulent Flow
Turbulent flow
Gas turbines
Streamlines
Finite Element
Petrov-Galerkin
Formulation
Computing
Galerkin methods
Turbulent Combustion
Engines
Stabilized Finite Elements
Petrov-Galerkin Method
Aeroengine
Diffusivity
Flame
Temperature Field

ASJC Scopus subject areas

  • Ocean Engineering
  • Mechanical Engineering
  • Computational Theory and Mathematics
  • Computational Mathematics
  • Applied Mathematics

これを引用

A DRD finite element formulation for computing turbulent reacting flows in gas turbine combustors. / Corsini, A.; Iossa, C.; Rispoli, F.; Tezduyar, Tayfun E.

:: Computational Mechanics, 巻 46, 番号 1, 06.2010, p. 159-167.

研究成果: Article

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