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bound.f
executable file
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bound.f
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! Part of Dflow3d a 3D Navier Stokes solver with variable density for
! simulations of near field dredge plume mixing
! Copyright (C) 2012 Lynyrd de Wit
! This program is free software: you can redistribute it and/or modify
! it under the terms of the GNU General Public License as published by
! the Free Software Foundation, either version 3 of the License, or
! (at your option) any later version.
! 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, see <http://www.gnu.org/licenses/>.
subroutine bound(Ubound,Vbound,Wbound,rho,botstress,tt,Ub1in,Vb1in,Wb1in,Ub2in,Vb2in,Wb2in,Ub3in,Vb3in,Wb3in)
USE nlist
implicit none
c
! include 'param.txt'
! include 'common.txt'
c
integer jtmp,t
c
real Ubound(0:i1,0:j1,0:k1),Vbound(0:i1,0:j1,0:k1),rho(0:i1,0:j1,0:k1),
+ Wbound(0:i1,0:j1,0:k1)
real ubb(0:i1,0:k1),val,theta,Ubc,Vbc,Wbc,xx,yy,r_orifice2,Wjet,theta_U,theta_V
real vbb(0:i1,0:k1)
real wbb(0:i1,0:k1)
real ubf(0:i1,0:k1)
real vbf(0:i1,0:k1)
real wbf(0:i1,0:k1)
real cbf(0:i1,0:k1)
real cbb(0:i1,0:k1)
real ust_U_b,ust_V_b,Chezy,fluc,f,tt,z0_U,z0_V,phi
integer botstress,n,jbeg,jend
real Ub1(0:i1,0:k1),Vb1(0:i1,0:k1),Wb1(0:i1,0:k1),Ub2(0:j1,0:k1),Vb2(0:j1+1,0:k1),Wb2(0:j1,0:k1)
real,intent(in) :: Ub1in(0:i1,0:k1),Vb1in(0:i1,0:k1),Wb1in(0:i1,0:k1),Ub2in(0:j1,0:k1),Vb2in(0:j1+1,0:k1),Wb2in(0:j1,0:k1)
real,intent(in) :: Ub3in(0:i1,0:j1),Vb3in(0:i1,0:j1),Wb3in(0:i1,0:j1)
real x,y,z!,u(1:kmax-2),v(1:kmax-2),w(1:kmax-2),zz(1:kmax-2)
real Wbc1,Wbc2!,Ubc1,Vbc1
real Ujetbc,Vjetbc,Wjetbc,Ujetbc2,Vjetbc2
real rr,interpseries
real Ujet2,zzz,z2,val2,jetcorr
integer i_inflowU,i_inflowVW,i_outflowU,i_outflowVW,i_shift
real outflow_factor
! pi = 4.0 * atan(1.0)
c
c
c*************************************************************
c
c Subroutine bound sets the boundary conditions for all variables,
c except for the diffusion coefficients. These are set in submod.
c The common boundary conditions for the pressure are set in mkgrid.
c
c*************************************************************
c
c*************************************************************
c Ubc,Vbc,Wbc are boundary velocities in carthesian
c x,y,z coordinate system, not in r,theta,z like this code
! rotation ship for ambient side current
if (LOA<0.) then
phi=0. !don't rotate grid
else
if ((U_TSHD-U_b).eq.0) then
phi=atan2(V_b,1.e-12)
else
phi=atan2(V_b,(U_TSHD-U_b))
endif
endif
c influence of waves on lateral boundaries:
! 10-3-2020 noted that perhaps exact location wave inflow bc is not consistent with staggered layout near boundary, have to research later [Ub1in,Vb1in,Wb1in are defined at Uloc; Ub2in,Vb2in,Wb2in are defined at Vloc; but Ub1,Vb1,Wb1,Ub2,Vb2,Wb2 defined at u,v,w loc respectively and they are added without correcting
! 24-6-2024: Test to remove wave flow component on lateral boundaries. Wave flow boundary conditions on lateral xy-boundaries can give trouble with the sediment mass balance because waves can result in negative outflow at x=xmax but this is overruled in the code for stability, but as a result the influx of sediment is not taken into account which results in loss of sediment in the CFD domain over time.
IF(.false.) THEN
! IF(Hs>0.) THEN
DO k=0,k1
DO i=0,i1
IF (rank.eq.0) THEN
j=0
ELSE ! also for rank between 0 and px-1 now Ub1 is filled, but this is not used anyways
j=jmax
ENDIF
z=(k-0.5)*dz-zbed(i,j)
z=MIN(z,depth-zbed(i,j))
z=MAX(z,0.)
z2=k*dz-zbed(i,j)
z2=MIN(z2,depth-zbed(i,j))
z2=MAX(z2,0.)
val=z/(ABS(z)+1e-12)*cosh(kabs_w*z)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
val2=sinh(kabs_w*z2)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
! force val to zero when under obstacle height, val2 is automatically
x=Ru(i)*cos_u(j)-schuif_x
y=Ru(i)*sin_u(j)
Ub1(i,k)=Ub1in(i,k)+kx_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_v(j)-schuif_x
y=Rp(i)*sin_v(j)
Vb1(i,k)=Vb1in(i,k)+ky_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_u(j)-schuif_x
y=Rp(i)*sin_u(j)
Wb1(i,k)=Wb1in(i,k)+val2*sin(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
ENDDO
DO j=0,j1
IF (periodicx.eq.3.or.periodicx.eq.4) THEN
i=i1
ELSE
if (monopile>0) then !inflow Ubc2,Vbc2 defined at imax instead at i=0
i=imax
elseif((U_b.ge.0.and.LOA<0).or.((U_TSHD-U_b).ge.0.and.LOA>0.)) THEN
i=0
else !inflow Ubc2,Vbc2 defined at imax instead at i=0
i=imax
endif
ENDIF
z=(k-0.5)*dz-zbed(i,j)
z=MIN(z,depth-zbed(i,j))
z=MAX(z,0.)
z2=k*dz-zbed(i,j)
z2=MIN(z2,depth-zbed(i,j))
z2=MAX(z2,0.)
val=z/(ABS(z)+1e-12)*cosh(kabs_w*z)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
val2=sinh(kabs_w*z2)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
! force val to zero when under obstacle height, val2 is automatically
x=Ru(i)*cos_u(j)-schuif_x
y=Ru(i)*sin_u(j)
Ub2(j,k)=Ub2in(j,k)+kx_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_v(j)-schuif_x
y=Rp(i)*sin_v(j)
Vb2(j,k)=Vb2in(j,k)+ky_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_u(j)-schuif_x
y=Rp(i)*sin_u(j)
Wb2(j,k)=Wb2in(j,k)+val2*sin(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
ENDDO
ENDDO
Vb2(j1+1,:)=Vb2(j1,:)
ELSE
Ub1=Ub1in
Vb1=Vb1in
Wb1=Wb1in
Ub2=Ub2in
Vb2=Vb2in
Wb2=Wb2in
ENDIF
!c get stuff from other CPU's
call shiftf(Ubound,ubf)
call shiftf(Vbound,vbf)
call shiftf(Wbound,wbf)
call shiftb(Ubound,ubb)
call shiftb(Vbound,vbb)
call shiftb(Wbound,wbb)
Wbc1=W_b
if (periodicy.eq.0) then
if (rank.eq.0) then ! boundaries in j-direction
! write(*,*),'rank (moet 0 zijn)',rank
j=0
do k=1,kmax
do i=1,imax
if (bcfile.ne.'') then
Ubc1(i,k)=Ubcoarse1(i,k)
Vbc1(i,k)=Vbcoarse1(i,k)
Wbc1=Wbcoarse1(i,k)
endif
Ubc=0.5*(Ub1(i,k)+Ub1(i+1,k))+Ubc1(i,k)
Vbc=Vb1(i,k)+Vbc1(i,k)
Wbc=0.5*(Wb1(i,k)+Wb1(i,k+1))+Wbc1
Ubound(i,0,k) = Ubc*cos_u(0)+Vbc*sin_u(0) !Ubf(i,k)
! Ubound(i,0,k) = 2.*(Ubc*cos_u(0)+Vbc*sin_u(0))-Ubound(i,1,k) !Ubf(i,k)
Vbound(i,0,k) = -Ubc*sin_v(0)+Vbc*cos_v(0) !Vbf(i,k)
! Vbound(i,0,k) = 2.*(-Ubc*sin_v(0)+Vbc*cos_v(0))-Vbound(i,1,k) !Vbf(i,k)
Wbound(i,0,k) = Wbc !2.*Wbc-Wbound(i,1,k)!Wbc !Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
elseif (rank.eq.px-1) then
! write(*,*),'rank (moet px-1 zijn)',rank
j=jmax
do k=1,kmax
do i=1,imax
if (bcfile.ne.'') then
Ubc1(i,k)=Ubcoarse1(i,k)
Vbc1(i,k)=Vbcoarse1(i,k)
Wbc1=Wbcoarse1(i,k)
endif
Ubc=0.5*(Ub1(i,k)+Ub1(i+1,k))+Ubc1(i,k)
Vbc=Vb1(i,k)+Vbc1(i,k)
Wbc=0.5*(Wb1(i,k)+Wb1(i,k+1))+Wbc1
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubc*cos_u(j1)+Vbc*sin_u(j1) !Ubb(i,k)
! Ubound(i,j1,k) =2.*(Ubc*cos_u(j1)+Vbc*sin_u(j1))-Ubound(i,jmax,k) !Ubb(i,k)
Vbound(i,jmax,k) =-Ubc*sin_v(jmax)+Vbc*cos_v(jmax) !Vbb(i,k)
Vbound(i,j1,k) = Vbound(i,jmax,k)
! Vbound(i,jmax,k) =2.*(-Ubc*sin_v(jmax)+Vbc*cos_v(jmax))-Vbound(i,jmax-1,k) !Vbb(i,k)
Wbound(i,j1,k) = Wbc !2.*Wbc-Wbound(i,jmax,k) !Wbb(i,k)
enddo
enddo
else
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
endif
elseif (periodicy.eq.1) then !periodic in y:
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
elseif (periodicy.eq.2) then !free slip lateral boundaries
if (rank.eq.0) then ! boundaries in j-direction
j=0
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubound(i,1,k)
Vbound(i,0,k) = 0.
Wbound(i,0,k) = Wbound(i,1,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
elseif (rank.eq.px-1) then
! write(*,*),'rank (moet px-1 zijn)',rank
j=jmax
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubound(i,jmax,k)
Vbound(i,jmax,k) = 0.
Vbound(i,j1,k) = 0.
Wbound(i,j1,k) = Wbound(i,jmax,k)
enddo
enddo
else
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
endif
endif
! Ubc1=0.
! Vbc1=0.
Wbc1=W_b
if (periodicx.eq.0.and.monopile.eq.-1) then
if((U_b.ge.0.and.LOA<0).or.((U_TSHD-U_b).ge.0.and.LOA>0.)) THEN
i_inflowU=0
i_inflowVW=0
i_outflowU=imax
i_outflowVW=i1
i_shift=-1
outflow_factor=1.
else !inflow Ubc2,Vbc2 defined at imax instead at i=0
i_inflowU=imax
i_inflowVW=i1
i_outflowU=0
i_outflowVW=0
i_shift=+1
outflow_factor=-1.
endif
if (Uoutflow.eq.2) then ! convective outflow boundary
do k=1,kmax ! boundaries in i-direction
do j=0,j1
Wbc2=0.
if (bcfile.ne.'') then
Ubc2(j,k)=Ubcoarse2(j,k)
Vbc2(j,k)=Vbcoarse2(j,k)
Wbc2=Wbcoarse2(j,k)
endif
Ubc=Ub2(j,k)+Ubc2(j,k)
Vbc=0.5*(Vb2(j,k)+Vb2(j+1,k))+Vbc2(j,k)
Wbc=0.5*(Wb2(j,k)+Wb2(j,k+1))+Wbc2
Ubound(i_inflowU,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Vbound(i_inflowVW,j,k) = (-Ubc*sin_v(j)+Vbc*cos_v(j)) !2.*(-Ubc*sin_v(j)+Vbc*cos_v(j))-Vbound(1,j,k)
Wbound(i_inflowVW,j,k) = Wbc !2.*Wbc - Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)
Ubc = outflow_factor*MAX(outflow_factor*Ubc2(j,k)*cos_u(j)+outflow_factor*Vbc2(j,k)*sin_u(j),0.) !Unormal outflow boundary at U-loc; should be >0 otherwise no outflow and divide by zero
! Ubound(imax,j,k) = MAX(Ubound(imax-1,j,k)-dr(imax)/(Ubc*dt)*(Unew(imax-1,j,k)-Uold(imax-1,j,k)),0.)
! Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
! Vbound(i1,j,k) = Vbound(imax,j,k)-(Rp(i1)-Rp(imax))/(Ubc*dt)*(Vnew(imax,j,k)-Vold(imax,j,k))
! Wbound(i1,j,k) = Wbound(imax,j,k)-(Rp(i1)-Rp(imax))/(Ubc*dt)*(Wnew(imax,j,k)-Wold(imax,j,k))
! solving Ui+1^n+1-Ui+1^n)/dt+Unormal(Ui+1^n+1-Ui^n+1)/dx=0. !implicit treatment of dUdn term
!Ubound(imax,j,k) = (Unew(imax,j,k)+Ubc*dt/dr(imax)*Ubound(imax-1,j,k))/(1.+Ubc*dt/dr(imax))
!Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
!Vbound(i1,j,k) = (Vnew(i1,j,k)+Ubc*dt/(Rp(i1)-Rp(imax))*Vbound(imax,j,k))/(1.+Ubc*dt/(Rp(i1)-Rp(imax)))
!Wbound(i1,j,k) = (Wnew(i1,j,k)+Ubc*dt/(Rp(i1)-Rp(imax))*Wbound(imax,j,k))/(1.+Ubc*dt/(Rp(i1)-Rp(imax)))
Ubound(i_outflowVW,j,k) = outflow_factor*MAX(outflow_factor*Ubound(i_outflowVW+i_shift,j,k),0.)
Ubound(i_outflowU,j,k) = (Unew(i_outflowU,j,k)+Ubc*dt/dr(i_outflowU)*Ubound(i_outflowU+i_shift,j,k))
& /(1.+Ubc*dt/dr(i_outflowU))
Vbound(i_outflowVW,j,k) = (Vnew(i_outflowVW,j,k)+Ubc*dt/dr(i_outflowVW)*Vbound(i_outflowVW+i_shift,j,k))
& /(1.+Ubc*dt/dr(i_outflowVW))
Wbound(i_outflowVW,j,k) = (Wnew(i_outflowVW,j,k)+Ubc*dt/dr(i_outflowVW)*Wbound(i_outflowVW+i_shift,j,k))
& /(1.+Ubc*dt/dr(i_outflowVW))
enddo
enddo
else !Neumann outflow boundary
do k=1,kmax ! boundaries in i-direction
do j=0,j1
Wbc2=0.
if (bcfile.ne.'') then
Ubc2(j,k)=Ubcoarse2(j,k)
Vbc2(j,k)=Vbcoarse2(j,k)
Wbc2=Wbcoarse2(j,k)
endif
Ubc=Ub2(j,k)+Ubc2(j,k)
Vbc=0.5*(Vb2(j,k)+Vb2(j+1,k))+Vbc2(j,k)
Wbc=0.5*(Wb2(j,k)+Wb2(j,k+1))+Wbc2
Ubound(i_inflowU,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Ubound(i_outflowU,j,k) = outflow_factor*MAX(outflow_factor*Ubound(i_outflowU+i_shift,j,k),0.)
Ubound(i_outflowVW,j,k) = outflow_factor*MAX(outflow_factor*Ubound(i_outflowVW+i_shift,j,k),0.)
Vbound(i_inflowVW,j,k) = (-Ubc*sin_v(j)+Vbc*cos_v(j)) !2.*(-Ubc*sin_v(j)+Vbc*cos_v(j))-Vbound(1,j,k)
Vbound(i_outflowVW,j,k) = Vbound(i_outflowVW+i_shift,j,k)
Wbound(i_inflowVW,j,k) = Wbc !2.*Wbc - Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)
Wbound(i_outflowVW,j,k) = Wbound(i_outflowVW+i_shift,j,k)
enddo
enddo
endif
elseif (periodicx.eq.0.and.monopile>0) then ! closed boundary at i=0 (flow past circular cylinder); mixed inflow/outflow bc at imax; monopile=1=partial slip with tau-wall monopile2=free slip
if (monopile.eq.4) then !no slip monopile wall
do k=1,kmax
do j=0,j1
Ubound(0,j,k) = 0.
Vbound(0,j,k) = -Vbound(1,j,k)
Wbound(0,j,k) = -Wbound(1,j,k)
enddo
enddo
else
do k=1,kmax
do j=0,j1
Ubound(0,j,k) = 0.
Vbound(0,j,k) = Vbound(1,j,k)
Wbound(0,j,k) = Wbound(1,j,k)
enddo
enddo
endif
if (rank.le.CEILING(REAL(px)/4.)-1) then ! first 1/4 of domain is outflow bc
jend = CEILING(REAL(jmax*px)*0.25) !end of first 1/4 global j-index
jend = MIN(jend-rank*jmax,j1) !end of first 1/4 local j-index
if (Uoutflow.eq.2) then ! convective outflow boundary
do j=0,jend
do k=1,kmax
Ubc = MAX(Ubc2(j,k)*cos_u(j)+Vbc2(j,k)*sin_u(j),0.) !Unormal outflow boundary at U-loc; should be >0 otherwise no outflow and divide by zero
!if (k.eq.1) write(*,*),'rank,j,Ubc',rank,j,Ubc
! Wbound(i1,j,k) = Wbound(imax,j,k)-(Rp(i1)-Rp(imax))/(Ubc*dt)*(Wnew(imax,j,k)-Wold(imax,j,k))
! Ubound(imax,j,k) = MAX(Ubound(imax-1,j,k)-dr(imax)/(Ubc*dt)*(Unew(imax-1,j,k)-Uold(imax-1,j,k)),0.)
! Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
! Vbound(i1,j,k) = Vbound(imax,j,k)-(Rp(i1)-Rp(imax))/(Ubc*dt)*(Vnew(imax,j,k)-Vold(imax,j,k))
! solving Ui+1^n+1-Ui+1^n)/dt+Unormal(Ui+1^n+1-Ui^n+1)/dx=0. !implicit treatment of dUdn term
Ubound(imax,j,k) = (Unew(imax,j,k)+Ubc*dt/dr(imax)*Ubound(imax-1,j,k))/(1.+Ubc*dt/dr(imax))
Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
Vbound(i1,j,k) = (Vnew(i1,j,k)+Ubc*dt/(Rp(i1)-Rp(imax))*Vbound(imax,j,k))/(1.+Ubc*dt/(Rp(i1)-Rp(imax)))
Wbound(i1,j,k) = (Wnew(i1,j,k)+Ubc*dt/(Rp(i1)-Rp(imax))*Wbound(imax,j,k))/(1.+Ubc*dt/(Rp(i1)-Rp(imax)))
enddo
enddo
else !Neumann outflow
do j=0,jend
do k=1,kmax
Ubound(imax,j,k) = MAX(Ubound(imax-1,j,k),0.)
Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
Vbound(i1,j,k) = Vbound(imax,j,k)
Wbound(i1,j,k) = Wbound(imax,j,k)
enddo
enddo
endif
do j=jend+1,j1 !remainder belongs to second 1/4 of domain is inflow
do k=1,kmax
Wbc2=0.
if (bcfile.ne.'') then
Ubc2(j,k)=Ubcoarse2(j,k)
Vbc2(j,k)=Vbcoarse2(j,k)
Wbc2=Wbcoarse2(j,k)
endif
Ubc=Ub2(j,k)+Ubc2(j,k)
Vbc=0.5*(Vb2(j,k)+Vb2(j+1,k))+Vbc2(j,k)
Wbc=0.5*(Wb2(j,k)+Wb2(j,k+1))+Wbc2
Ubound(imax,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Ubound(i1,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Vbound(i1,j,k) = (-Ubc*sin_v(j)+Vbc*cos_v(j)) !2.*(-Ubc*sin_v(j)+Vbc*cos_v(j))-Vbound(1,j,k)
Wbound(i1,j,k) = Wbc !2.*Wbc - Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)
enddo
enddo
elseif (rank.ge.px-CEILING(REAL(px)/4.)-1) then ! last 1/4 of domain is outflow bc
jbeg = jmax*px - CEILING(REAL(jmax*px)*0.25) ! begin of last 1/4 global j-index
jbeg = MAX(jbeg-rank*jmax,0) !begin of last 1/4 local j-index
if (Uoutflow.eq.2) then ! convective outflow boundary
do j=jbeg,j1 ! outflow
do k=1,kmax
Ubc = MAX(Ubc2(j,k)*cos_u(j)+Vbc2(j,k)*sin_u(j),0.) !Unormal outflow boundary at U-loc; should be >0 otherwise no outflow and divide by zero
! if (k.eq.1) write(*,*),'rank,j,Ubc',rank,j,Ubc
! Ubound(imax,j,k) = MAX(Ubound(imax-1,j,k)-dr(imax)/(Ubc*dt)*(Unew(imax-1,j,k)-Uold(imax-1,j,k)),0.)
! Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
! Vbound(i1,j,k) = Vbound(imax,j,k)-(Rp(i1)-Rp(imax))/(Ubc*dt)*(Vnew(imax,j,k)-Vold(imax,j,k))
! Wbound(i1,j,k) = Wbound(imax,j,k)-(Rp(i1)-Rp(imax))/(Ubc*dt)*(Wnew(imax,j,k)-Wold(imax,j,k))
! solving Ui+1^n+1-Ui+1^n)/dt+Unormal(Ui+1^n+1-Ui^n+1)/dx=0. !implicit treatment of dUdn term
Ubound(imax,j,k) = (Unew(imax,j,k)+Ubc*dt/dr(imax)*Ubound(imax-1,j,k))/(1.+Ubc*dt/dr(imax))
Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
Vbound(i1,j,k) = (Vnew(i1,j,k)+Ubc*dt/(Rp(i1)-Rp(imax))*Vbound(imax,j,k))/(1.+Ubc*dt/(Rp(i1)-Rp(imax)))
Wbound(i1,j,k) = (Wnew(i1,j,k)+Ubc*dt/(Rp(i1)-Rp(imax))*Wbound(imax,j,k))/(1.+Ubc*dt/(Rp(i1)-Rp(imax)))
enddo
enddo
else !Neumann outflow condition
do j=jbeg,j1 ! outflow
do k=1,kmax
Ubound(imax,j,k) = MAX(Ubound(imax-1,j,k),0.)
Ubound(i1,j,k) = MAX(Ubound(imax,j,k),0.)
Vbound(i1,j,k) = Vbound(imax,j,k)
Wbound(i1,j,k) = Wbound(imax,j,k)
enddo
enddo
endif
do j=0,MIN(j1,jbeg-1) !remainder belongs to second 1/4 of domain is inflow
do k=1,kmax
Wbc2=0.
if (bcfile.ne.'') then
Ubc2(j,k)=Ubcoarse2(j,k)
Vbc2(j,k)=Vbcoarse2(j,k)
Wbc2=Wbcoarse2(j,k)
endif
Ubc=Ub2(j,k)+Ubc2(j,k)
Vbc=0.5*(Vb2(j,k)+Vb2(j+1,k))+Vbc2(j,k)
Wbc=0.5*(Wb2(j,k)+Wb2(j,k+1))+Wbc2
Ubound(imax,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Ubound(i1,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Vbound(i1,j,k) = (-Ubc*sin_v(j)+Vbc*cos_v(j)) !2.*(-Ubc*sin_v(j)+Vbc*cos_v(j))-Vbound(1,j,k)
Wbound(i1,j,k) = Wbc !2.*Wbc - Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)
enddo
enddo
else !middle 2/4 is inflow bc
do j=0,j1 !remainder belongs to second 1/4 of domain is inflow
do k=1,kmax
Wbc2=0.
if (bcfile.ne.'') then
Ubc2(j,k)=Ubcoarse2(j,k)
Vbc2(j,k)=Vbcoarse2(j,k)
Wbc2=Wbcoarse2(j,k)
endif
Ubc=Ub2(j,k)+Ubc2(j,k)
Vbc=0.5*(Vb2(j,k)+Vb2(j+1,k))+Vbc2(j,k)
Wbc=0.5*(Wb2(j,k)+Wb2(j,k+1))+Wbc2
Ubound(imax,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Ubound(i1,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
Vbound(i1,j,k) = (-Ubc*sin_v(j)+Vbc*cos_v(j)) !2.*(-Ubc*sin_v(j)+Vbc*cos_v(j))-Vbound(1,j,k)
Wbound(i1,j,k) = Wbc !2.*Wbc - Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)
enddo
enddo
endif
elseif (periodicx.eq.2) then ! no outflow in x direction:
do k=1,kmax
do j=0,j1
Ubound(0,j,k) = 0.
Ubound(imax,j,k) = 0.
Ubound(i1,j,k) = 0.
Vbound(0,j,k) = -Vbound(1,j,k)
Vbound(i1,j,k) = -Vbound(imax,j,k)
Wbound(0,j,k) = -Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)
Wbound(i1,j,k) = 2.*W_ox - Wbound(imax,j,k)
enddo
enddo
else ! periodic in x:
do k=1,kmax
do j=0,j1
Ubound(0,j,k) = Ubound(imax,j,k)
Ubound(i1,j,k) = Ubound(1,j,k)
Vbound(0,j,k) = Vbound(imax,j,k)
Vbound(i1,j,k) = Vbound(1,j,k)
Wbound(0,j,k) = Wbound(imax,j,k)
Wbound(i1,j,k) = Wbound(1,j,k)
enddo
enddo
endif
if (botstress.eq.-2) then
do j=0,j1 ! boundaries in k-direction
do i=0,i1
Ubound(i,j,k1) = -Ubound(i,j,kmax)
Vbound(i,j,k1) = -Vbound(i,j,kmax)
!Wbound(i,j,kmax) = 0.
Wbound(i,j,k1) = 0.
Ubound(i,j,0) = -Ubound(i,j,1)
Vbound(i,j,0) = -Vbound(i,j,1)
Wbound(i,j,0) = Wbed(i,j) !0.
xx=Rp(i)*cos_u(j)-schuif_x
yy=Rp(i)*sin_u(j)
Wbound(i,j,kmax)=(om_w+kx_w*U_TSHD*cos(phi)+ky_w*U_TSHD*sin(phi))*Hs/2.
& *sin(kx_w*(xx-U_TSHD*cos(phi)*tt)+ky_w*(yy-U_TSHD*sin(phi)*tt)-om_w*tt)
enddo
enddo
elseif (botstress.eq.-1) then
do j=0,j1 ! boundaries in k-direction
do i=0,i1
Ubound(i,j,k1) = Ubound(i,j,kmax)
Vbound(i,j,k1) = Vbound(i,j,kmax)
!Wbound(i,j,kmax) = 0.
Wbound(i,j,k1) = 0.
Ubound(i,j,0) = -Ubound(i,j,1)
Vbound(i,j,0) = -Vbound(i,j,1)
Wbound(i,j,0) = Wbed(i,j) !0.
xx=Rp(i)*cos_u(j)-schuif_x
yy=Rp(i)*sin_u(j)
Wbound(i,j,kmax)=(om_w+kx_w*U_TSHD*cos(phi)+ky_w*U_TSHD*sin(phi))*Hs/2.
& *sin(kx_w*(xx-U_TSHD*cos(phi)*tt)+ky_w*(yy-U_TSHD*sin(phi)*tt)-om_w*tt)
enddo
enddo
else
do j=0,j1 ! boundaries in k-direction
do i=0,i1
Ubound(i,j,k1) = Ubound(i,j,kmax)
Vbound(i,j,k1) = Vbound(i,j,kmax)
!Wbound(i,j,kmax) = 0.
Wbound(i,j,k1) = 0.
Ubound(i,j,0) = Ubound(i,j,1)
Vbound(i,j,0) = Vbound(i,j,1)
Wbound(i,j,0) = Wbed(i,j) !0.
xx=Rp(i)*cos_u(j)-schuif_x
yy=Rp(i)*sin_u(j)
Wbound(i,j,kmax)=(om_w+kx_w*U_TSHD*cos(phi)+ky_w*U_TSHD*sin(phi))*Hs/2.
& *sin(kx_w*(xx-U_TSHD*cos(phi)*tt)+ky_w*(yy-U_TSHD*sin(phi)*tt)-om_w*tt)
enddo
enddo
endif
!! Set boundary conditions vertical jet in:
if (plumetseriesfile.eq.'') then
Wjet=W_j
f=Strouhal*ABS(W_j)/MAX(radius_j*2.,1.e-12) !Strouholt number is 0.3
else
Wjet=interpseries(plumetseries,plumeUseries,plumeseriesloc,tt)
W_j=Wjet
f=Strouhal*ABS(W_j)/MAX(radius_j*2.,1.e-12) !Strouholt number is 0.3
endif
jetcorr=pi/(2.*pi*(1/(1./W_j_powerlaw+1)-1./(1./W_j_powerlaw+2.))) !=1.22449 for W_j_powerlaw=7
do t=1,tmax_inPpunt
i=i_inPpunt(t)
j=j_inPpunt(t)
fluc=0.
do n=1,azi_n
fluc=fluc+sin(2.*pi*f*tt/n+azi_angle_p(i,j))
enddo
xx=Rp(i)*cos_u(j)-schuif_x
yy=Rp(i)*sin_u(j)
rr=1.-sqrt((xx**2+yy**2)/MAX(radius_j**2,1.e-12))
rr=MAX(rr,0.)
if (outflow_overflow_down.eq.1) then
Wbound(i,j,kmax)=jetcorr*Wjet*rr**(1./W_j_powerlaw)+Awjet/REAL(azi_n)*Wjet*fluc !no turb SEM fluc
else
Wbound(i,j,kmax)=jetcorr*Wjet*rr**(1./W_j_powerlaw)+Awjet/REAL(azi_n)*Wjet*fluc+Wb3in(i,j) !including turb SEM fluc
endif
! Wbound(i,j,k1)=jetcorr*Wjet*rr**(1./W_j_powerlaw)+Awjet/REAL(azi_n)*Wjet*fluc
enddo
do t=1,tmax_inUpunt
i=i_inUpunt(t)
j=j_inUpunt(t)
fluc=0.
do n=1,azi_n
fluc=fluc+sin(2.*pi*f*tt/n+azi_angle_u(i,j))
enddo
Ujetbc=Aujet/azi_n*Wjet*fluc
Vjetbc=Avjet/azi_n*Wjet*fluc
if (outflow_overflow_down.eq.1) then
Ujetbc2=Ujetbc*cos(azi_angle_u(i,j))-Vjetbc*sin(azi_angle_u(i,j)) !no turb SEM fluc
Vjetbc2=Ujetbc*sin(azi_angle_u(i,j))+Vjetbc*cos(azi_angle_u(i,j))
else
Ujetbc2=Ujetbc*cos(azi_angle_u(i,j))-Vjetbc*sin(azi_angle_u(i,j))+Ub3in(i,j) !including turb SEM fluc
Vjetbc2=Ujetbc*sin(azi_angle_u(i,j))+Vjetbc*cos(azi_angle_u(i,j))+Vb3in(i,j)
endif
Ubound(i,j,k1)=2.*(Ujetbc2*cos_u(j)+Vjetbc2*sin_u(j))-Ubound(i,j,kmax) !(Aujet/6.*Wjet*fluc)
enddo
do t=1,tmax_inVpunt
i=i_inVpunt(t)
j=j_inVpunt(t)
fluc=0.
do n=1,azi_n
fluc=fluc+sin(2.*pi*f*tt/n+azi_angle_v(i,j))
enddo
Ujetbc=Aujet/azi_n*Wjet*fluc
Vjetbc=Avjet/azi_n*Wjet*fluc
if (outflow_overflow_down.eq.1) then
Ujetbc2=Ujetbc*cos(azi_angle_v(i,j))-Vjetbc*sin(azi_angle_v(i,j)) !no turb SEM fluc
Vjetbc2=Ujetbc*sin(azi_angle_v(i,j))+Vjetbc*cos(azi_angle_v(i,j))
else
Ujetbc2=Ujetbc*cos(azi_angle_v(i,j))-Vjetbc*sin(azi_angle_v(i,j))+Ub3in(i,j) !including turb SEM fluc
Vjetbc2=Ujetbc*sin(azi_angle_v(i,j))+Vjetbc*cos(azi_angle_v(i,j))+Vb3in(i,j) !including turb SEM fluc
endif
Vbound(i,j,k1)=2.*(Ujetbc2*sin_v(j)+Vjetbc2*cos_v(j))-Vbound(i,j,kmax) !(Aujet/6.*Wjet*fluc)
enddo
!! Set boundary conditions horizontal jet2 in:
if (plumetseriesfile2.eq.'') then
Ujet2=U_j2
f=Strouhal*ABS(U_j2)/(radius_j2*2.) !Strouholt number is 0.3
else
Ujet2=interpseries(plumetseries2,plumeUseries2,plumeseriesloc2,tt)
U_j2=Ujet2
f=Strouhal2*ABS(U_j2)/(radius_j2*2.) !Strouholt number is 0.3
endif
do t=1,tmax_inPpunt2
k=k_inPpunt2(t)
j=j_inPpunt2(t)
zzz=k*dz-0.5*dz-zjet2
yy=Rp(0)*sin_u(j)
fluc=0.
do n=1,azi_n2
fluc=fluc+sin(2.*pi*f*tt/n+atan2(zzz,yy))
enddo
rr=1.-sqrt((zzz**2+yy**2)/radius_j2**2)
rr=MAX(rr,0.)
Ujetbc=jetcorr*Ujet2*rr**(1./W_j_powerlaw)+Aujet2/azi_n2*Ujet2*fluc
Vjetbc=Avjet/azi_n*Ujet2*fluc
Ubound(0,j,k)=(Ujetbc*cos_u(j)+Vjetbc*sin_u(j))
enddo
do t=1,tmax_inWpunt2
k=k_inWpunt2(t)
j=j_inWpunt2(t)
zzz=k*dz-zjet2
yy=Rp(0)*sin_u(j)
fluc=0.
do n=1,azi_n
fluc=fluc+sin(2.*pi*f*tt/n+atan2(zzz,yy))
enddo
Wjetbc=Awjet/azi_n*Ujet2*fluc
Vjetbc=Avjet/azi_n*Ujet2*fluc
Wbound(0,j,k)=2.*(cos(atan2(zzz,yy))*Wjetbc+sin(atan2(zzz,yy))*Vjetbc)-Wbound(1,j,k)
enddo
do t=1,tmax_inVpunt2
k=k_inVpunt2(t)
j=j_inVpunt2(t)
zzz=k*dz-0.5*dz-zjet2
yy=Rp(0)*sin_v(j)
rr=1.-sqrt((zzz**2+yy**2)/MAX(radius_j**2,1.e-12))
rr=MAX(rr,0.)
fluc=0.
do n=1,azi_n
fluc=fluc+sin(2.*pi*f*tt/n+atan2(zzz,yy))
enddo
Ujetbc=Ujet2*rr**(1./W_j_powerlaw)+Aujet2/azi_n2*Ujet2*fluc
Vjetbc=Avjet/azi_n*Ujet2*fluc
Wjetbc=Awjet/azi_n*Ujet2*fluc
Vbound(0,j,k)=2.*((-Ujetbc*sin_v(j)+Vjetbc*cos_v(j))*cos(atan2(zzz,yy))-sin(atan2(zzz,yy))*Wjetbc)-Vbound(1,j,k)
enddo
do t=1,tmax_inWpunt_suction ! add suction in front of draghead
k=k_inWpunt_suction(t)
j=j_inWpunt_suction(t)
i=i_inWpunt_suction(t)
Wjetbc=pi*MAX(radius_j**2,1.e-12)*W_j*perc_dh_suction/(dr(i)*3.*Dsp) !(m3/s)/m2=m/s per suction cell (perc_dh_suction is corrected for number of dragheads)
Wbound(i,j,k)=Wjetbc
enddo
if (i_periodicx>0) then
do k=0,k1
do j=0,j1
Ubound(0,j,k) = Ubound(i_periodicx,j,k)
Vbound(0,j,k) = Vbound(i_periodicx,j,k)
Wbound(0,j,k) = Wbound(i_periodicx,j,k)
enddo
enddo
endif
end
subroutine bound_incljet(Ubound,Vbound,Wbound,rho,botstress,tt,Ub1in,Vb1in,Wb1in,Ub2in,Vb2in,Wb2in,Ub3in,Vb3in,Wb3in)
USE nlist
implicit none
c
! include 'param.txt'
! include 'common.txt'
c
integer jtmp,t,inout,im,jm
real xTSHD(1:4),yTSHD(1:4)
c
real Ubound(0:i1,0:j1,0:k1),Vbound(0:i1,0:j1,0:k1),rho(0:i1,0:j1,0:k1),
+ Wbound(0:i1,0:j1,0:k1)
real ubb(0:i1,0:k1),val,theta,Ubc,Vbc,Wbc,xx,yy,r_orifice2,Wjet,theta_U,theta_V
real vbb(0:i1,0:k1)
real wbb(0:i1,0:k1)
real ubf(0:i1,0:k1)
real vbf(0:i1,0:k1)
real wbf(0:i1,0:k1)
real cbf(0:i1,0:k1)
real cbb(0:i1,0:k1)
real ust_U_b,ust_V_b,Chezy,fluc,f,tt,z0_U,z0_V,phi
integer botstress,n,jp
real Ub1(0:i1,0:k1),Vb1(0:i1,0:k1),Wb1(0:i1,0:k1),Ub2(0:j1,0:k1),Vb2(0:j1+1,0:k1),Wb2(0:j1,0:k1)
real,intent(in):: Ub1in(0:i1,0:k1),Vb1in(0:i1,0:k1),Wb1in(0:i1,0:k1),Ub2in(0:j1,0:k1),Vb2in(0:j1+1,0:k1),Wb2in(0:j1,0:k1)
real,intent(in) :: Ub3in(0:i1,0:j1),Vb3in(0:i1,0:j1),Wb3in(0:i1,0:j1)
real x,y,z
real Wbc1,Wbc2
real Ujetbc,Vjetbc,Wjetbc,Ujetbc2,Vjetbc2
real rr,interpseries
real uu1,uu2,vv1,vv2
real zzz,Ujet2,z2,val2,jetcorr
integer kp,kpp,kb,tel,jbeg,jend
real zb_W,zb_U,zb_V,vel_ibm2,distance_to_bed_kp,distance_to_bed_kpp,yplus,absU,z0,ust
real Ubound2(0:i1,0:j1,0:k1),Vbound2(0:i1,0:j1,0:k1),Wbound2(0:i1,0:j1,0:k1)
integer i_inflowU,i_inflowVW,i_outflowU,i_outflowVW,i_shift
real outflow_factor
! pi = 4.0 * atan(1.0)
c
c
c*************************************************************
c
c Subroutine bound sets the boundary conditions for all variables,
c except for the diffusion coefficients. These are set in submod.
c The common boundary conditions for the pressure are set in mkgrid.
c
c*************************************************************
c
c*************************************************************
c Ubc,Vbc,Wbc are boundary velocities in carthesian
c x,y,z coordinate system, not in r,theta,z like this code
! rotation ship for ambient side current
if (LOA<0.) then
phi=0. !don't rotate grid
else
if ((U_TSHD-U_b).eq.0) then
phi=atan2(V_b,1.e-12)
else
phi=atan2(V_b,(U_TSHD-U_b))
endif
endif
c influence of waves on lateral boundaries:
! 24-6-2024: Test to remove wave flow component on lateral boundaries. Wave flow boundary conditions on lateral xy-boundaries can give trouble with the sediment mass balance because waves can result in negative outflow at x=xmax but this is overruled in the code for stability, but as a result the influx of sediment is not taken into account which results in loss of sediment in the CFD domain over time.
IF(.false.) THEN
! IF(Hs>0.) THEN
DO k=0,k1
DO i=0,i1
IF (rank.eq.0) THEN
j=0
ELSE ! also for rank between 0 and px-1 now Ub1 is filled, but this is not used anyways
j=jmax
ENDIF
z=(k-0.5)*dz-zbed(i,j)
z=MIN(z,depth-zbed(i,j))
z=MAX(z,0.)
z2=k*dz-zbed(i,j)
z2=MIN(z2,depth-zbed(i,j))
z2=MAX(z2,0.)
val=z/(ABS(z)+1e-12)*cosh(kabs_w*z)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
val2=sinh(kabs_w*z2)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
! force val to zero when under obstacle height, val2 is automatically
x=Ru(i)*cos_u(j)-schuif_x
y=Ru(i)*sin_u(j)
Ub1(i,k)=Ub1in(i,k)+kx_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_v(j)-schuif_x
y=Rp(i)*sin_v(j)
Vb1(i,k)=Vb1in(i,k)+ky_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_u(j)-schuif_x
y=Rp(i)*sin_u(j)
Wb1(i,k)=Wb1in(i,k)+val2*sin(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
ENDDO
DO j=0,j1
IF (periodicx.eq.3.or.periodicx.eq.4) THEN
i=i1
ELSE
if (monopile>0) then !inflow Ubc2,Vbc2 defined at imax instead at i=0
i=imax
elseif((U_b.ge.0.and.LOA<0).or.((U_TSHD-U_b).ge.0.and.LOA>0.)) THEN
i=0
else !inflow Ubc2,Vbc2 defined at imax instead at i=0
i=imax
endif
ENDIF
z=(k-0.5)*dz-zbed(i,j)
z=MIN(z,depth-zbed(i,j))
z=MAX(z,0.)
z2=k*dz-zbed(i,j)
z2=MIN(z2,depth-zbed(i,j))
z2=MAX(z2,0.)
val=z/(ABS(z)+1e-12)*cosh(kabs_w*z)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
val2=sinh(kabs_w*z2)/sinh(kabs_w*(depth-zbed(i,j)))*(om_w-kx_w*U_w-ky_w*V_w)*Hs/2.
! force val to zero when under obstacle height, val2 is automatically
x=Ru(i)*cos_u(j)-schuif_x
y=Ru(i)*sin_u(j)
Ub2(j,k)=Ub2in(j,k)+kx_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_v(j)-schuif_x
y=Rp(i)*sin_v(j)
Vb2(j,k)=Vb2in(j,k)+ky_w/kabs_w*val*cos(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
x=Rp(i)*cos_u(j)-schuif_x
y=Rp(i)*sin_u(j)
Wb2(j,k)=Wb2in(j,k)+val2*sin(kx_w*(x-U_TSHD*cos(phi)*tt)+ky_w*(y-U_TSHD*sin(phi)*tt)-om_w*tt)
ENDDO
ENDDO
Vb2(j1+1,:)=Vb2(j1,:)
ELSE
Ub1=Ub1in
Vb1=Vb1in
Wb1=Wb1in
Ub2=Ub2in
Vb2=Vb2in
Wb2=Wb2in
ENDIF
!c get stuff from other CPU's
call shiftf(Ubound,ubf)
call shiftf(Vbound,vbf)
call shiftf(Wbound,wbf)
call shiftb(Ubound,ubb)
call shiftb(Vbound,vbb)
call shiftb(Wbound,wbb)
Wbc1=W_b
if (periodicy.eq.0) then
if (rank.eq.0) then ! boundaries in j-direction
! write(*,*),'rank (moet 0 zijn)',rank
j=0
do k=1,kmax
do i=1,imax
if (bcfile.ne.'') then
Ubc1(i,k)=Ubcoarse1(i,k)
Vbc1(i,k)=Vbcoarse1(i,k)
Wbc1=Wbcoarse1(i,k)
endif
Ubc=0.5*(Ub1(i,k)+Ub1(i+1,k))+Ubc1(i,k)
Vbc=Vb1(i,k)+Vbc1(i,k)
Wbc=0.5*(Wb1(i,k)+Wb1(i,k+1))+Wbc1
Ubound(i,0,k) = Ubc*cos_u(0)+Vbc*sin_u(0) !Ubf(i,k)
! Ubound(i,0,k) = 2.*(Ubc*cos_u(0)+Vbc*sin_u(0))-Ubound(i,1,k) !Ubf(i,k)
Vbound(i,0,k) = -Ubc*sin_v(0)+Vbc*cos_v(0) !Vbf(i,k)
! Vbound(i,0,k) = 2.*(-Ubc*sin_v(0)+Vbc*cos_v(0))-Vbound(i,1,k) !Vbf(i,k)
Wbound(i,0,k) = Wbc !2.*Wbc-Wbound(i,1,k)!Wbc !Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
elseif (rank.eq.px-1) then
! write(*,*),'rank (moet px-1 zijn)',rank
j=jmax
do k=1,kmax
do i=1,imax
if (bcfile.ne.'') then
Ubc1(i,k)=Ubcoarse1(i,k)
Vbc1(i,k)=Vbcoarse1(i,k)
Wbc1=Wbcoarse1(i,k)
endif
Ubc=0.5*(Ub1(i,k)+Ub1(i+1,k))+Ubc1(i,k)
Vbc=Vb1(i,k)+Vbc1(i,k)
Wbc=0.5*(Wb1(i,k)+Wb1(i,k+1))+Wbc1
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubc*cos_u(j1)+Vbc*sin_u(j1) !Ubb(i,k)
! Ubound(i,j1,k) =2.*(Ubc*cos_u(j1)+Vbc*sin_u(j1))-Ubound(i,jmax,k) !Ubb(i,k)
Vbound(i,jmax,k) =-Ubc*sin_v(jmax)+Vbc*cos_v(jmax) !Vbb(i,k)
Vbound(i,j1,k) = Vbound(i,jmax,k)
! Vbound(i,jmax,k) =2.*(-Ubc*sin_v(jmax)+Vbc*cos_v(jmax))-Vbound(i,jmax-1,k) !Vbb(i,k)
Wbound(i,j1,k) = Wbc !2.*Wbc-Wbound(i,jmax,k) !Wbb(i,k)
enddo
enddo
else
! write(*,*),'rank (moet geen 0 of px zijn)',rank
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
endif
elseif (periodicy.eq.1) then !periodic in y:
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
elseif (periodicy.eq.2) then !free slip lateral boundaries
if (rank.eq.0) then ! boundaries in j-direction
j=0
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubound(i,1,k)
Vbound(i,0,k) = 0.
Wbound(i,0,k) = Wbound(i,1,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
elseif (rank.eq.px-1) then
! write(*,*),'rank (moet px-1 zijn)',rank
j=jmax
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubound(i,jmax,k)
Vbound(i,jmax,k) = 0.
Vbound(i,j1,k) = Vbound(i,jmax,k)
Wbound(i,j1,k) = Wbound(i,jmax,k)
enddo
enddo
else
do k=1,kmax
do i=1,imax
Ubound(i,0,k) = Ubf(i,k)
Vbound(i,0,k) = Vbf(i,k)
Wbound(i,0,k) = Wbf(i,k)
Ubound(i,j1,k) =Ubb(i,k)
Vbound(i,j1,k) =Vbb(i,k)
Wbound(i,j1,k) =Wbb(i,k)
enddo
enddo
endif
endif
Wbc1=W_b
if (periodicx.eq.0.and.monopile.eq.-1) then
if((U_b.ge.0.and.LOA<0).or.((U_TSHD-U_b).ge.0.and.LOA>0.)) THEN
i_inflowU=0
i_inflowVW=0
i_outflowU=imax
i_outflowVW=i1
i_shift=-1
outflow_factor=1.
else !inflow Ubc2,Vbc2 defined at imax instead at i=0
i_inflowU=imax
i_inflowVW=i1
i_outflowU=0
i_outflowVW=0
i_shift=+1
outflow_factor=-1.
endif
if (Uoutflow.eq.2) then ! convective outflow boundary
do k=1,kmax ! boundaries in i-direction
do j=0,j1
Wbc2=0.
if (bcfile.ne.'') then
Ubc2(j,k)=Ubcoarse2(j,k)
Vbc2(j,k)=Vbcoarse2(j,k)
Wbc2=Wbcoarse2(j,k)
endif
Ubc=Ub2(j,k)+Ubc2(j,k)
Vbc=0.5*(Vb2(j,k)+Vb2(j+1,k))+Vbc2(j,k)
Wbc=0.5*(Wb2(j,k)+Wb2(j,k+1))+Wbc2
! Ubound(0,j,k) = Ubc*cos_u(j)+Vbc*sin_u(j)
! Vbound(0,j,k) = (-Ubc*sin_v(j)+Vbc*cos_v(j)) !2.*(-Ubc*sin_v(j)+Vbc*cos_v(j))-Vbound(1,j,k)
! Wbound(0,j,k) = Wbc !2.*Wbc - Wbound(1,j,k) !Wbound(0,j,k) = Wbc !- Wbound(1,j,k)