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Code_Saturne
CFD tool
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Solving the for incompressible flows or slightly compressible flows for one time step.
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Functions/Subroutines | |
subroutine | turbke |
Solving the for incompressible flows or slightly compressible flows for one time step.
subroutine turbke | ( | ) |
[in] | nvar | total number of variables |
[in] | nscal | total number of scalars |
[in] | ncepdp | number of cells with head loss |
[in] | ncesmp | number of cells with mass source term |
[in] | icepdc | index of the ncepdp cells with head loss |
[in] | icetsm | index of cells with mass source term |
[in] | itypsm | mass source type for the variables (cf. ustsma) |
[in] | dt | time step (per cell) |
[in,out] | rtp | calculated variables at cell centers (at the current time step) |
[in] | rtpa | calculated variables at cell centers (at the previous time step) |
[in] | propce | physical properties at cell centers |
[in] | propfa | physical properties at interior face centers |
[in] | propfb | physical properties at boundary face centers |
[in] | tslagr | coupling term of the lagangian module |
[in] | coefa,coefb | boundary conditions |
[in] | ckupdc | work array for the head loss |
[in] | smacel | values of the variables associated to the mass source (for ivar=ipr, smacel is the mass flux) |
[in] | prdv2f | production term stored for the v2f |