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Variables
Specific arrays for the coupled case
Collaboration diagram for Specific arrays for the coupled case:

Variables

integer, dimension(:), allocatable itypfb
 
integer, dimension(:), allocatable itrifb
 indirection array allowing to sort the boundary faces according to their boundary condition type itypfb More...
 
integer, dimension(:), allocatable izfppp
 to identify boundary zones associated with boundary faces (particular physics) More...
 
integer, dimension(:), allocatable izfrad
 to identify boundary zones associated with boundary faces (radiative transfert) More...
 
integer, dimension(:), allocatable ifapat
 number of the wall face (type itypfb=iparoi or iparug) which is closest to the center of a given volume when necessary ( $R_{ij}-\varepsilon$ with wall echo, LES with van Driest-wall damping, or $k-\omega$ (SST) turbulence model) and when icdpar=2. The number of the wall face which is the closest to the center of the cell iel is ifapat(iel1). This calculation method is not compatible with parallelism and periodicity More...
 
integer, dimension(:), allocatable idfstr
 the index of the structure, (idfstr(ifac) where ifac is the index of the face), 0 if the face is not coupled to any structure. More...
 
double precision, dimension(:),
allocatable 
s2kw
 square of the norm of the deviatoric part of the deformation rate tensor ( $S^2=2S_{ij}^D S_{ij}^D$). This array is defined only with the $k-\omega$ (SST) turbulence model More...
 
double precision, dimension(:),
allocatable 
divukw
 divergence of the velocity. More precisely it is the trace of the velocity gradient (and not a finite volume divergence term). In the cell iel, $div(\vect{u})$ is given by divukw(iel1). This array is defined only with the $k-\omega$ SST turbulence model (because in this case it may be calculated at the same time as $S^2$) More...
 
double precision, dimension(:,:),
allocatable 
straio
 strain rate tensor at the previous time step More...
 

Detailed Description

Variable Documentation

double precision, dimension(:), allocatable divukw

divergence of the velocity. More precisely it is the trace of the velocity gradient (and not a finite volume divergence term). In the cell iel, $div(\vect{u})$ is given by divukw(iel1). This array is defined only with the $k-\omega$ SST turbulence model (because in this case it may be calculated at the same time as $S^2$)

integer, dimension(:), allocatable idfstr

the index of the structure, (idfstr(ifac) where ifac is the index of the face), 0 if the face is not coupled to any structure.

integer, dimension(:), allocatable ifapat

number of the wall face (type itypfb=iparoi or iparug) which is closest to the center of a given volume when necessary ( $R_{ij}-\varepsilon$ with wall echo, LES with van Driest-wall damping, or $k-\omega$ (SST) turbulence model) and when icdpar=2. The number of the wall face which is the closest to the center of the cell iel is ifapat(iel1). This calculation method is not compatible with parallelism and periodicity

integer, dimension(:), allocatable itrifb

indirection array allowing to sort the boundary faces according to their boundary condition type itypfb

integer, dimension(:), allocatable itypfb

boundary condition type at the boundary face ifac (see user subroutine cs_user_boundary_conditions)

integer, dimension(:), allocatable izfppp

to identify boundary zones associated with boundary faces (particular physics)

integer, dimension(:), allocatable izfrad

to identify boundary zones associated with boundary faces (radiative transfert)

double precision, dimension(:), allocatable s2kw

square of the norm of the deviatoric part of the deformation rate tensor ( $S^2=2S_{ij}^D S_{ij}^D$). This array is defined only with the $k-\omega$ (SST) turbulence model

double precision, dimension(:,:), allocatable straio

strain rate tensor at the previous time step