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

CASE IVa

CASE IVa

 

SST k-w

CASE IVb

CASE IVb

 

CASE IVc

CASE IVc

 

 

Spalart & Allmaras

CASE Va

CASE Va

 

SST k-w

CASE Vb

CASE Vb

 

CASE Vc

CASE Vc

 

 

Spalart & Allmaras

CASE VIa

CASE VIa

 

SST k-w

CASE VIb

CASE VIb

 

CASE VIc

CASE VIc