Performance of Reynolds-averaged turbulence models for transonic flow around airfoil

Kentaro Hara, Ken Ichi Abe

Research output: Contribution to journalArticle

Abstract

In this study, four Reynolds-averaged eddy-viscosity turbulence models (a linear κ - ε, a linear κ - ω, a nonlinear - and a nonlinear -) were applied to a transonic flow around an airfoil, being called 'ONERA M6 wing'. The particular concern was focused on the model performance under various grid resolutions in the vicinity of wall surface. Computed results were compared with each other and the corresponding experimental data and the model performance was discussed in detail.

Original languageEnglish
Pages (from-to)447-453
Number of pages7
JournalProgress in Computational Fluid Dynamics
Volume8
Issue number7-8
DOIs
Publication statusPublished - Dec 3 2008

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Transonic flow
transonic flow
airfoils
turbulence models
Turbulence models
Airfoils
eddy viscosity
wings
grids
Viscosity

All Science Journal Classification (ASJC) codes

  • Condensed Matter Physics
  • Computer Science Applications

Cite this

Performance of Reynolds-averaged turbulence models for transonic flow around airfoil. / Hara, Kentaro; Abe, Ken Ichi.

In: Progress in Computational Fluid Dynamics, Vol. 8, No. 7-8, 03.12.2008, p. 447-453.

Research output: Contribution to journalArticle

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