Authors: Kentaro Hara, Ken-ichi Abe
Addresses: Department of Aeronautics and Astronautics, Kyushu University, Motooka, Nishi-ku, Fukuoka 819-0395, Japan. ' Department of Aeronautics and Astronautics, Kyushu University, Motooka, Nishi-ku, Fukuoka 819-0395, Japan
Abstract: In this study, four Reynolds-averaged eddy-viscosity turbulence models (a linear κ – ω, a linear κ – ω, a nonlinear κ – ε and a nonlinear κ – ω) 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.
Keywords: turbulence modelling; Reynolds-averaged turbulence model; shock wave; transonic flow; nonlinear eddy-viscosity model; airfoils; Reynolds-averaged Navier-Stokes; RANS models.
Progress in Computational Fluid Dynamics, An International Journal, 2008 Vol.8 No.7/8, pp.447 - 453
Published online: 19 Nov 2008 *Full-text access for editors Access for subscribers Purchase this article Comment on this article