|  | programmer's documentation | 
| Variables | |
| integer | nscamx | 
| maximum number of scalars solutions of an advection equation, apart from the variables of the turbulence model  ) , that is to say the temperature and other scalars (passive or not, user-defined or not)  More... | |
| integer | nvarmx | 
| maximal number of variables = nscamx + 12 (u,v,w,P,Rij,e,alp)  More... | |
| integer | nprcmx | 
| maximal number of physical properties at cells. = nscamx (Lambda) + 7 (rho,Cp,viscl,visct,cou,fou,iprtot) + 4 (estim)  More... | |
| integer | nprfmx | 
| maximal number of physical properties at internal faces. = nscamx (flumas) + 2*(flumas,alp)  More... | |
| integer | nprbmx | 
| maximal number of physical properties at external faces. = nscamx (flumab) + 3*(flumab,alp, romb)  More... | |
| integer | npromx | 
| maximal number of physical properties, increased by nprcmx. They will be stored in the arrays propceMore... | |
| integer | ngrdmx | 
| maximal number of physical quantities = nvarmx + npromx  More... | |
| integer | nsmamx | 
| maximal size of mass source terms arrays. (= nvarmx + 1 for smacel)  More... | |
| integer | nvppmx | 
| number of displayed variables. = ngrdmx + 20 (20 > dt, tpucou, increased by 16 ...)  More... | |
| integer | ntypmx | 
| Maximal possible boundary condition types.  More... | |
| integer | iindef | 
| pointer for undefined type face (non-standard case)  More... | |
| integer | ientre | 
| if itypfb=ientre: inlet face.  More... | |
| integer | isolib | 
| if itypfb=isolib: free outlet face (or more precisely free inlet/outlet with forced pressure)  More... | |
| integer | isymet | 
| if itypfb=isymet: symmetry face (or wall without friction).  More... | |
| integer | iparoi | 
| if itypfb=iparoi: smooth solid wall face, impermeable and with friction.  More... | |
| integer | iparug | 
| if itypfb=iparug: rough solid wall face, impermeable and with friction.  More... | |
| integer | iesicf | 
| if itypfb=iesicf: imposed inlet/outlet for compressible flow (for example, supersonic inlet).  More... | |
| integer | isspcf | 
| if itypfb=isspcf: supersonic outlet for compressible flow.  More... | |
| integer | isopcf | 
| if itypfb=isopcf: mixed outlet for compressible flow with a given pressure.  More... | |
| integer | iephcf | 
| if itypfb=isopcf: mixed inlet for compressible flow with given total pressure and total enthalpy (reservoir boundary conditions).  More... | |
| integer | ieqhcf | 
| integer | icscpl | 
| integer | ifrent | 
| if itypfb=ifrent: free entrance based on Bernoulli equation when the flow is incoming, standard outlet when outgoing  More... | |
| integer | nestmx | 
| maximal number of valuators for Navier-Stokes  More... | |
| integer | iespre | 
| error estimator for Navier-Stokes. iest = iespre: prediction, (default name: EsPre). After the velocity prediction step (yielding  ), the estimator  , local variable calculated at every cell  , is created from  , which represents the residual of the equation solved during this step:  and  : 
 | |
| integer | iesder | 
| error estimator for Navier-Stokes. iest = iesder: drift (default name: EsDer). The estimator  is based on the following quantity (intrinsic to the code): 
 | |
| integer | iescor | 
| error estimator for Navier-Stokes. iest = iescor: correction, (default name: EsCor). The estimator  comes directly from the mass flow calculated with the updated velocity field: 
 | |
| integer | iestot | 
| error estimator for Navier-Stokes. iest = iestot: total, (default name: EsTot). The estimator  , local variable calculated at every cell  , is based on the quantity  , which represents the residual of the equation using the updated values of  and  : 
 | |
| integer | nbmomx | 
| maximum number of calculated time-averages (default value: 50)  More... | |
| integer | ndgmox | 
| maximum degree of the time-averages (default value: 5)  More... | |
| integer | ibfixe | 
| boundary condition type for mesh velocity in ALE: fixed wall  More... | |
| integer | igliss | 
| boundary condition type for mesh velocity in ALE: sliding wall  More... | |
| integer | ivimpo | 
| boundary condition type for mesh velocity in ALE: imposed velocity.  More... | |
| integer | ifresf | 
| boundary condition type for mesh velocity in ALE for modelling free surface (  ).  More... | |
| integer | nstrmx | 
| maximum number of structures in ALE  More... | |
| integer ibfixe | 
boundary condition type for mesh velocity in ALE: fixed wall
| integer icscpl | 
| integer ientre | 
if itypfb=ientre: inlet face.
| integer iephcf | 
if itypfb=isopcf: mixed inlet for compressible flow with given total pressure and total enthalpy (reservoir boundary conditions).
| integer ieqhcf | 
| integer iescor | 
error estimator for Navier-Stokes. iest = iescor: correction, (default name: EsCor). The estimator  comes directly from the mass flow calculated with the updated velocity field:
 comes directly from the mass flow calculated with the updated velocity field: 
 
 are taken at the cell centers, the divergence is calculated after projection on the faces.
 are taken at the cell centers, the divergence is calculated after projection on the faces.  represents the Kronecker symbol.
 represents the Kronecker symbol. .
.| integer iesder | 
error estimator for Navier-Stokes. iest = iesder: drift (default name: EsDer). The estimator  is based on the following quantity (intrinsic to the code):
 is based on the following quantity (intrinsic to the code): 
 
| integer iesicf | 
if itypfb=iesicf: imposed inlet/outlet for compressible flow (for example, supersonic inlet).
| integer iespre | 
error estimator for Navier-Stokes. iest = iespre: prediction, (default name: EsPre). After the velocity prediction step (yielding  ), the estimator
), the estimator  , local variable calculated at every cell
, local variable calculated at every cell  , is created from
, is created from  , which represents the residual of the equation solved during this step:
, which represents the residual of the equation solved during this step:  and
 and  :
: 
 

 which intrinsicly appears with the norm
 which intrinsicly appears with the norm  .
. . The size of the cell therefore appears in its calculation and induces a weighting effect.
. The size of the cell therefore appears in its calculation and induces a weighting effect. is ideally equal to zero when the reconstruction methods are perfect and the associated system is solved exactly.
 is ideally equal to zero when the reconstruction methods are perfect and the associated system is solved exactly. | integer iestot | 
error estimator for Navier-Stokes. iest = iestot: total, (default name: EsTot). The estimator  , local variable calculated at every cell
, local variable calculated at every cell  , is based on the quantity
, is based on the quantity  , which represents the residual of the equation using the updated values of
, which represents the residual of the equation using the updated values of  and
 and  :
: 
 

 expressed at the cell centres (and not taken from the updated mass flow at the faces).
 expressed at the cell centres (and not taken from the updated mass flow at the faces). which intrinsicly appears with the norm
 which intrinsicly appears with the norm  .
. . The size of the cell therefore appears in its calculation and induces a weighting effect.
. The size of the cell therefore appears in its calculation and induces a weighting effect. | integer ifrent | 
if itypfb=ifrent: free entrance based on Bernoulli equation when the flow is incoming, standard outlet when outgoing
| integer ifresf | 
boundary condition type for mesh velocity in ALE for modelling free surface (  ).
). 
| integer igliss | 
boundary condition type for mesh velocity in ALE: sliding wall
| integer iindef | 
pointer for undefined type face (non-standard case)
| integer iparoi | 
if itypfb=iparoi: smooth solid wall face, impermeable and with friction.
| integer iparug | 
if itypfb=iparug: rough solid wall face, impermeable and with friction.
| integer isolib | 
if itypfb=isolib: free outlet face (or more precisely free inlet/outlet with forced pressure)
 . The pressure is set to
. The pressure is set to  at the first isolib face met. The pressure calibration is always done on a single face, even if there are several outlets.
 at the first isolib face met. The pressure calibration is always done on a single face, even if there are several outlets.| integer isopcf | 
if itypfb=isopcf: mixed outlet for compressible flow with a given pressure.
| integer isspcf | 
if itypfb=isspcf: supersonic outlet for compressible flow.
| integer isymet | 
if itypfb=isymet: symmetry face (or wall without friction).
| integer ivimpo | 
boundary condition type for mesh velocity in ALE: imposed velocity.
| integer nbmomx | 
maximum number of calculated time-averages (default value: 50)
| integer ndgmox | 
maximum degree of the time-averages (default value: 5)
| integer nestmx | 
maximal number of valuators for Navier-Stokes
| integer ngrdmx | 
maximal number of physical quantities = nvarmx + npromx
| integer nprbmx | 
maximal number of physical properties at external faces. = nscamx (flumab) + 3*(flumab,alp, romb)
| integer nprcmx | 
maximal number of physical properties at cells. = nscamx (Lambda) + 7 (rho,Cp,viscl,visct,cou,fou,iprtot) + 4 (estim)
| integer nprfmx | 
maximal number of physical properties at internal faces. = nscamx (flumas) + 2*(flumas,alp)
| integer npromx | 
maximal number of physical properties, increased by nprcmx. They will be stored in the arrays propce 
| integer nscamx | 
maximum number of scalars solutions of an advection equation, apart from the variables of the turbulence model  ) , that is to say the temperature and other scalars (passive or not, user-defined or not)
) , that is to say the temperature and other scalars (passive or not, user-defined or not) 
| integer nsmamx | 
maximal size of mass source terms arrays. (= nvarmx + 1 for smacel)
| integer nstrmx | 
maximum number of structures in ALE
| integer ntypmx | 
Maximal possible boundary condition types.
| integer nvarmx | 
maximal number of variables = nscamx + 12 (u,v,w,P,Rij,e,alp)
| integer nvppmx | 
number of displayed variables. = ngrdmx + 20 (20 > dt, tpucou, increased by 16 ...)
 1.8.3.1
 1.8.3.1