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

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

研究成果: Article査読

56 被引用数 (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.

本文言語English
ページ(範囲)159-167
ページ数9
ジャーナルComputational Mechanics
46
1
DOI
出版ステータスPublished - 2010 6
外部発表はい

ASJC Scopus subject areas

  • 計算力学
  • 海洋工学
  • 機械工学
  • 計算理論と計算数学
  • 計算数学
  • 応用数学

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