# Solve UV.f90 - Solution of the momentum equations for U and V

(Difference between revisions)
 Revision as of 08:50, 3 May 2010 (view source)Michail (Talk | contribs) (New page:
!Sample program for solving Lid-driven cavity flow test using SIMPLE-algorithm ! solution of momentum equation for U and V modul !Copyright (C) 2010  Michail Kiričkov  !This progra...)← Older edit                                                                           Revision as of 13:34, 4 May 2010 (view source)Michail  (Talk | contribs) Newer edit →
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! upwind differencing (all other will be included into the source term)                                                                                         ! upwind differencing (all other will be included into the source term)

-                                                                                                                                                                                                                                                                                                Conv_w = Area_w *  ( F(i,j,1) + F(i-1,j  ,1) ) * 0.5                     +                                                                                      Conv_w = Area_w *  ( F(i,j,1) + F(i-1,j  ,1) ) * 0.5
-                                                                                                                                                                                                                                                                                                Conv_e = Area_e *  ( F(i,j,1) + F(i+1,j  ,1) ) * 0.5                     +                                                                                      Conv_e = Area_e *  ( F(i,j,1) + F(i+1,j  ,1) ) * 0.5
Conv_s = Area_s *  ( F(i,j,2) + F(i  ,j-1,2) ) * 0.5                                                                                                            Conv_s = Area_s *  ( F(i,j,2) + F(i  ,j-1,2) ) * 0.5
Conv_n = Area_n *  ( F(i,j,2) + F(i  ,j+1,2) ) * 0.5                                                                                                            Conv_n = Area_n *  ( F(i,j,2) + F(i  ,j+1,2) ) * 0.5
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if(i.eq.2    )Conv_w = 0.                                                                                                                                       if(i.eq.2    )Conv_w = 0.
if(i.eq.NXmax)Conv_e = 0.                                                                                                                                       if(i.eq.NXmax)Conv_e = 0.
-                                                                                                                                                                                                                                                                                                if(j.eq.2    )Conv_s = 0.                                                +                                                                                      if(j.eq.2    )Conv_s = 0.
if(j.eq.NYmax)Conv_n = 0.                                                                                                                                       if(j.eq.NYmax)Conv_n = 0.

## Revision as of 13:34, 4 May 2010

```
!Sample program for solving Lid-driven cavity flow test using SIMPLE-algorithm
! solution of momentum equation for U and V modul

!This program is free software; you can redistribute it and/or
!modify it under the terms of the GNU General Public License

!This program is distributed in the hope that it will be useful,
!but WITHOUT ANY WARRANTY; without even the implied warranty of
!MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
!GNU General Public License for more details.

!You should have received a copy of the GNU General Public License
!along with this program; if not, write to the Free Software
!Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.

!**********************************************************************
Subroutine Solve_UV
include 'icomm_1.f90'

!  calculation of fluxes
!  all geometry has rectangular 2D notation

Do 100 I= 2,NXmax
Do 100 J= 2,NYmax

Gam_e = ( Gam(i+1,j  ) + Gam(i  ,j  ) ) * 0.5
Gam_w = ( Gam(i-1,j  ) + Gam(i  ,j  ) ) * 0.5
Gam_s = ( Gam(i  ,j-1) + Gam(i  ,j  ) ) * 0.5
Gam_n = ( Gam(i  ,j+1) + Gam(i  ,j  ) ) * 0.5

!----------------------------------------------------
Area_w = Y(i-1,j)-Y(i-1,j-1)
Area_e = Y(i  ,j)-Y(i  ,j-1)

Area_s = X(i,j-1)-X(i-1,j-1)
Area_n = X(i,j  )-X(i-1,j  )
!----------------------------------------------------

Del_w  = Xc(i  ,j)-Xc(i-1,j)
Del_e  = Xc(i+1,j)-Xc(i  ,j)

Del_s  = Yc(i,j  )-Yc(i,j-1)
Del_n  = Yc(i,j+1)-Yc(i,j  )
!----------------------------------------------------

! upwind differencing (all other will be included into the source term)

Conv_w = Area_w *  ( F(i,j,1) + F(i-1,j  ,1) ) * 0.5
Conv_e = Area_e *  ( F(i,j,1) + F(i+1,j  ,1) ) * 0.5
Conv_s = Area_s *  ( F(i,j,2) + F(i  ,j-1,2) ) * 0.5
Conv_n = Area_n *  ( F(i,j,2) + F(i  ,j+1,2) ) * 0.5

if(i.eq.2    )Conv_w = 0.
if(i.eq.NXmax)Conv_e = 0.
if(j.eq.2    )Conv_s = 0.
if(j.eq.NYmax)Conv_n = 0.

Diff_e = Area_e * Gam_e / Del_e
Diff_w = Area_w * Gam_w / Del_w
Diff_s = Area_s * Gam_s / Del_s
Diff_n = Area_n * Gam_n / Del_n

Aw(i,j) = Diff_w + max(     Conv_w,0.)
Ae(i,j) = Diff_e + max(-1.* Conv_e,0.)
As(i,j) = Diff_s + max(     Conv_s,0.)
An(i,j) = Diff_n + max(-1.* Conv_n,0.)

Ap(i,j,1:2)= Aw(i,j) + Ae(i,j) + An(i,j) + As(i,j)

Sp(i,j,1:2)= 0.

!-------------------------------- HLPA SCHEME----------------------------
!  go to 600 ! (now HLPA is "off")

DO 500 nf=1,2

! Subroutine HLPA(Uw,Fww,Fw,Fp,Fe,Delta_f)

if( (i.GT.2).AND.(i.LT.NXmax-0).and.(j.GT.2).AND.(j.LT.NYmax-0) ) then

!------------------ w face -------------------
Fww = F(i-2,j,nf)
Fw  = F(i-1,j,nf)
Fp  = F(i  ,j,nf)
Fe  = F(i+1,j,nf)

call  HLPA(Conv_w,Fww,Fw,Fp,Fe,Delta_f)

Sp(i,j,nf) = Sp(i,j,nf) + Conv_w * Delta_f

!------------------ e face--------------------

Fww = F(i-1,j,nf)
Fw  = F(i  ,j,nf)
Fp  = F(i+1,j,nf)
Fe  = F(i+2,j,nf)

call  HLPA(Conv_e,Fww,Fw,Fp,Fe,Delta_f)

Sp(i,j,nf) = Sp(i,j,nf) + Conv_e * Delta_f * (-1.)

!------------------ s face--------------------
Fww = F(i  ,j-2,nf)
Fw  = F(i  ,j-1,nf)
Fp  = F(i  ,j  ,nf)
Fe  = F(i  ,j+1,nf)

call  HLPA(Conv_s,Fww,Fw,Fp,Fe,Delta_f)

Sp(i,j,nf) = Sp(i,j,nf) + Conv_s * Delta_f

!------------------ n face--------------------

Fww = F(i  ,j-1,nf)
Fw  = F(i  ,j  ,nf)
Fp  = F(i  ,j+1,nf)
Fe  = F(i  ,j+2,nf)

call  HLPA(Conv_n,Fww,Fw,Fp,Fe,Delta_f)

Sp(i,j,nf) = Sp(i,j,nf) + Conv_n * Delta_f *(-1.)

end if

500 continue

600 continue

!------------------------------------------------------------------------

100 continue ! coefficient cycle

Do 200 I= 2,NXmax
Do 200 J= 2,NYmax

DX = X(i,j) - X(i-1,j)
DY = Y(i,j) - Y(i,j-1)

VOL = DX * DY

PE = ( F(i,j,4) + F(i+1,j,4) ) * 0.5
PW = ( F(i,j,4) + F(i-1,j,4) ) * 0.5
PN = ( F(i,j,4) + F(i,j+1,4) ) * 0.5
PS = ( F(i,j,4) + F(i,j-1,4) ) * 0.5

DPx_c(i,j) = (PE-PW)/DX
DPy_c(i,j) = (PN-PS)/DY

Sp(i,j,1) = Sp(i,j,1) - DPx_c(i,j) * VOL
Sp(i,j,2) = Sp(i,j,2) - DPy_c(i,j) * VOL

200 continue

!---------------------------- under-relaxation ---------------------------------

Alfa = 0.85
Urf  = 1. / Alfa

Ap(1:NXmaxC,1:NYmaxC,1) = Ap(1:NXmaxC,1:NYmaxC,1)  * Urf
Sp(1:NXmaxC,1:NYmaxC,1) = Sp(1:NXmaxC,1:NYmaxC,1)  + (1. - Alfa )* Ap(1:NXmaxC,1:NYmaxC,1)*F(1:NXmaxC,1:NYmaxC,1) ! / Alfa

Ap(1:NXmaxC,1:NYmaxC,2) = Ap(1:NXmaxC,1:NYmaxC,2)  * Urf
Sp(1:NXmaxC,1:NYmaxC,2) = Sp(1:NXmaxC,1:NYmaxC,2)  + (1. - Alfa )* Ap(1:NXmaxC,1:NYmaxC,2)*F(1:NXmaxC,1:NYmaxC,2) ! / Alfa

!---------------------------------------------------------------------------------

!******************************************************************

niter = 0
write(*,*)'solve U'
call Convergence_Criteria(1,Res_sum_before)

10 continue
niter= niter + 1
Call TDMA_1(1)
call Convergence_Criteria(1,Res_sum_After)
If((abs(Res_sum_before-Res_sum_After).Ge.0.00000000001).and.niter.le.20)then

Res_sum_before = Res_sum_After
go to 10
End if

niter = 0
write(*,*)'solve V'
call Convergence_Criteria(2,Res_sum_before)

20	continue

niter= niter + 1
Call TDMA_1(2)
call Convergence_Criteria(2,Res_sum_After)
If((abs(Res_sum_before-Res_sum_After).Ge.0.00000000001).and.niter.le.20)then

Res_sum_before = Res_sum_After
go to 20
End if

!***********************************************************************

!---------------------------------------------------------------------------------
Return
End

```