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 |
|
||||
|
|
||||