Flow around a NACA 0012 airfoil

Available data

Each case is stored in a folder that contains sub-folders for each of the 6 grids sets available.

Folder of each case contains 15 files:

 File Contents README.txt Description of the contents of the other 15 files conv_data_cd.dat Friction () and pressure () drag coefficients and friction () and pressure () lift coefficients of the airfoils for the 6 grids available. conv_surface_cflo.dat Skin friction coefficient  at the 19 selected locations of the lower surface of the airfoil for the 6 grids available. conv_surface_cplo.dat Pressure coefficient  at the 19 selected locations of the lower surface of the airfoil for the 6 grids available. conv_surface_cfup.dat Skin friction coefficient  at the 19 selected locations of the upper surface of the airfoil for the 6 grids available. conv_surface_cplo.dat Pressure coefficient  at the 19 selected locations of the upper surface of the airfoil for the 6 grids available. field_points_r---.dat Horizontal  and vertical  velocity components and the eddy-viscosity  at the 130 selected field locations for each grid. r--- corresponds to the grid refinement ratio  as defined in the test case description. Reynolds number Turbulence Model Zipped Files Rar Files Spalart & Allmaras SST k-w Spalart & Allmaras SST k-w Spalart & Allmaras SST k-w