Summary A Large-eddy simulation version of the FLOWer code is introduced to compute attached flow around a quasi three-dimensional airfoil at a Mach number Ma = 0.088, Reynolds number Re = 8 × 105, and an angle of attack of 3.3°. For the treatment of the subgrid-scale stresses the MILES approach is chosen. The visualization of instantaneous flow fields shows the typical flow features such as the streaky structures in the near-wall region to be well resolved and the overall agreement of the computational results with experimental data to be satisfactory.
Large-Eddy Simulation of Attached Airfoil Flow
2005-01-01
10 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Large-Eddy Simulation of Attached Airfoil Flow
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