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advec_mom_kernel.f90
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advec_mom_kernel.f90
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!Crown Copyright 2012 AWE.
!
! This file is part of CloverLeaf.
!
! CloverLeaf 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.
!
! CloverLeaf 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
! CloverLeaf. If not, see http://www.gnu.org/licenses/.
!> @brief Fortran momentum advection kernel
!> @author Wayne Gaudin
!> @details Performs a second order advective remap on the vertex momentum
!> using van-Leer limiting and directional splitting.
!> Note that although pre_vol is only set and not used in the update, please
!> leave it in the method.
MODULE advec_mom_kernel_mod
CONTAINS
SUBROUTINE advec_mom_kernel(x_min,x_max,y_min,y_max, &
xvel1, &
yvel1, &
mass_flux_x, &
vol_flux_x, &
mass_flux_y, &
vol_flux_y, &
volume, &
density1, &
node_flux, &
node_mass_post, &
node_mass_pre, &
advec_vel, &
mom_flux, &
pre_vol, &
post_vol, &
celldx, &
celldy, &
which_vel, &
sweep_number, &
direction, &
vector )
IMPLICIT NONE
INTEGER :: x_min,x_max,y_min,y_max
INTEGER :: which_vel,sweep_number,direction
LOGICAL :: vector
REAL(KIND=8), TARGET,DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: xvel1,yvel1
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+2) :: mass_flux_x
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+2) :: vol_flux_x
REAL(KIND=8), DIMENSION(x_min-2:x_max+2,y_min-2:y_max+3) :: mass_flux_y
REAL(KIND=8), DIMENSION(x_min-2:x_max+2,y_min-2:y_max+3) :: vol_flux_y
REAL(KIND=8), DIMENSION(x_min-2:x_max+2,y_min-2:y_max+2) :: volume
REAL(KIND=8), DIMENSION(x_min-2:x_max+2,y_min-2:y_max+2) :: density1
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: node_flux
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: node_mass_post
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: node_mass_pre
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: advec_vel
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: mom_flux
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: pre_vol
REAL(KIND=8), DIMENSION(x_min-2:x_max+3,y_min-2:y_max+3) :: post_vol
REAL(KIND=8), DIMENSION(x_min-2:x_max+2) :: celldx
REAL(KIND=8), DIMENSION(y_min-2:y_max+2) :: celldy
INTEGER :: j,k,mom_sweep
INTEGER :: upwind,donor,downwind,dif
REAL(KIND=8) :: sigma,wind,width
REAL(KIND=8) :: sigma2,wind2
REAL(KIND=8) :: vdiffuw,vdiffdw,auw,adw,limiter
REAL(KIND=8) :: vdiffuw2,vdiffdw2,auw2,limiter2
REAL(KIND=8), POINTER, DIMENSION(:,:) :: vel1
! Choose the correct velocity, ideally, remove this pointer
! if it affects performance.
! Leave this one in as a test of performance
IF(which_vel.EQ.1)THEN
vel1=>xvel1
ELSE
vel1=>yvel1
ENDIF
mom_sweep=direction+2*(sweep_number-1)
!$OMP PARALLEL
IF(mom_sweep.EQ.1)THEN ! x 1
!$OMP DO
DO k=y_min-2,y_max+2
DO j=x_min-2,x_max+2
post_vol(j,k)= volume(j,k)+vol_flux_y(j ,k+1)-vol_flux_y(j,k)
pre_vol(j,k)=post_vol(j,k)+vol_flux_x(j+1,k )-vol_flux_x(j,k)
ENDDO
ENDDO
!$OMP END DO
ELSEIF(mom_sweep.EQ.2)THEN ! y 1
!$OMP DO
DO k=y_min-2,y_max+2
DO j=x_min-2,x_max+2
post_vol(j,k)= volume(j,k)+vol_flux_x(j+1,k )-vol_flux_x(j,k)
pre_vol(j,k)=post_vol(j,k)+vol_flux_y(j ,k+1)-vol_flux_y(j,k)
ENDDO
ENDDO
!$OMP END DO
ELSEIF(mom_sweep.EQ.3)THEN ! x 2
!$OMP DO
DO k=y_min-2,y_max+2
DO j=x_min-2,x_max+2
post_vol(j,k)=volume(j,k)
pre_vol(j,k)=post_vol(j,k)+vol_flux_y(j ,k+1)-vol_flux_y(j,k)
ENDDO
ENDDO
!$OMP END DO
ELSEIF(mom_sweep.EQ.4)THEN ! y 2
!$OMP DO
DO k=y_min-2,y_max+2
DO j=x_min-2,x_max+2
post_vol(j,k)=volume(j,k)
pre_vol(j,k)=post_vol(j,k)+vol_flux_x(j+1,k )-vol_flux_x(j,k)
ENDDO
ENDDO
!$OMP END DO
ENDIF
IF(direction.EQ.1)THEN
!$OMP DO
DO k=y_min,y_max+1
DO j=x_min-2,x_max+2
! Find staggered mesh mass fluxes, nodal masses and volumes.
node_flux(j,k)=0.25_8*(mass_flux_x(j,k-1 )+mass_flux_x(j ,k) &
+mass_flux_x(j+1,k-1)+mass_flux_x(j+1,k)) ! Mass Flux
ENDDO
ENDDO
!$OMP END DO
!$OMP DO
DO k=y_min,y_max+1
DO j=x_min-1,x_max+2
! Staggered cell mass post advection
node_mass_post(j,k)=0.25_8*(density1(j ,k-1)*post_vol(j ,k-1) &
+density1(j ,k )*post_vol(j ,k ) &
+density1(j-1,k-1)*post_vol(j-1,k-1) &
+density1(j-1,k )*post_vol(j-1,k ))
ENDDO
ENDDO
!$OMP END DO
!$OMP DO
DO k=y_min,y_max+1
DO j=x_min-1,x_max+2
! Stagered cell mass pre advection
node_mass_pre(j,k)=node_mass_post(j,k)-node_flux(j-1,k)+node_flux(j,k)
ENDDO
ENDDO
!$OMP END DO
IF(vector) THEN
!$OMP DO PRIVATE(sigma,width,limiter,vdiffuw,vdiffdw,auw,adw,wind &
!$OMP ,sigma2,limiter2,vdiffuw2,vdiffdw2,auw2,wind2)
DO k=y_min,y_max+1
DO j=x_min-1,x_max+1
sigma=ABS(node_flux(j,k))/(node_mass_pre(j+1,k))
sigma2=ABS(node_flux(j,k))/(node_mass_pre(j,k))
width=celldx(j)
vdiffuw=vel1(j+1,k)-vel1(j+2,k)
vdiffdw=vel1(j,k)-vel1(j+1,k)
vdiffuw2=vel1(j,k)-vel1(j-1,k)
vdiffdw2=-vdiffdw
auw=ABS(vdiffuw)
adw=ABS(vdiffdw)
auw2=ABS(vdiffuw2)
wind=1.0_8
wind2=1.0_8
IF(vdiffdw.LE.0.0) wind=-1.0_8
IF(vdiffdw2.LE.0.0) wind2=-1.0_8
limiter=wind*MIN(width*((2.0_8-sigma)*adw/width+(1.0_8+sigma)*auw/celldx(j+1))/6.0_8,auw,adw)
limiter2=wind2*MIN(width*((2.0_8-sigma2)*adw/width+(1.0_8+sigma2)*auw2/celldx(j-1))/6.0_8,auw2,adw)
IF(vdiffuw*vdiffdw.LE.0.0) limiter=0.0
IF(vdiffuw2*vdiffdw2.LE.0.0) limiter2=0.0
IF(node_flux(j,k).LT.0.0)THEN
advec_vel(j,k)=vel1(j+1,k)+(1.0-sigma)*limiter
ELSE
advec_vel(j,k)=vel1(j,k)+(1.0-sigma2)*limiter2
ENDIF
mom_flux(j,k)=advec_vel(j,k)*node_flux(j,k)
ENDDO
ENDDO
!$OMP END DO
ELSE
!$OMP DO PRIVATE(upwind,downwind,donor,dif,sigma,width,limiter,vdiffuw,vdiffdw,auw,adw,wind)
DO k=y_min,y_max+1
DO j=x_min-1,x_max+1
IF(node_flux(j,k).LT.0.0_8)THEN
upwind=j+2
donor=j+1
downwind=j
dif=donor
ELSE
upwind=j-1
donor=j
downwind=j+1
dif=upwind
ENDIF
sigma=ABS(node_flux(j,k))/(node_mass_pre(donor,k))
width=celldx(j)
vdiffuw=vel1(donor,k)-vel1(upwind,k)
vdiffdw=vel1(downwind,k)-vel1(donor,k)
limiter=0.0_8
IF(vdiffuw*vdiffdw.GT.0.0_8)THEN
auw=ABS(vdiffuw)
adw=ABS(vdiffdw)
wind=1.0_8
IF(vdiffdw.LE.0.0_8) wind=-1.0_8
limiter=wind*MIN(width*((2.0_8-sigma)*adw/width+(1.0_8+sigma)*auw/celldx(dif))/6.0_8,auw,adw)
ENDIF
advec_vel(j,k)=vel1(donor,k)+(1.0_8-sigma)*limiter
mom_flux(j,k)=advec_vel(j,k)*node_flux(j,k)
ENDDO
ENDDO
!$OMP END DO
ENDIF
!$OMP DO
DO k=y_min,y_max+1
DO j=x_min,x_max+1
vel1 (j,k)=(vel1 (j,k)*node_mass_pre(j,k)+mom_flux(j-1,k)-mom_flux(j,k))/node_mass_post(j,k)
ENDDO
ENDDO
!$OMP END DO
ELSEIF(direction.EQ.2)THEN
!$OMP DO
DO k=y_min-2,y_max+2
DO j=x_min,x_max+1
! Find staggered mesh mass fluxes and nodal masses and volumes.
node_flux(j,k)=0.25_8*(mass_flux_y(j-1,k )+mass_flux_y(j ,k ) &
+mass_flux_y(j-1,k+1)+mass_flux_y(j ,k+1))
ENDDO
ENDDO
!$OMP END DO
!$OMP DO
DO k=y_min-1,y_max+2
DO j=x_min,x_max+1
node_mass_post(j,k)=0.25_8*(density1(j ,k-1)*post_vol(j ,k-1) &
+density1(j ,k )*post_vol(j ,k ) &
+density1(j-1,k-1)*post_vol(j-1,k-1) &
+density1(j-1,k )*post_vol(j-1,k ))
ENDDO
ENDDO
!$OMP END DO
!$OMP DO
DO k=y_min-1,y_max+2
DO j=x_min,x_max+1
node_mass_pre(j,k)=node_mass_post(j,k)-node_flux(j,k-1)+node_flux(j,k)
ENDDO
ENDDO
!$OMP END DO
IF(vector) THEN
!$OMP DO PRIVATE(sigma,width,limiter,vdiffuw,vdiffdw,auw,adw,wind &
!$OMP ,sigma2,limiter2,vdiffuw2,vdiffdw2,auw2,wind2)
DO k=y_min-1,y_max+1
DO j=x_min,x_max+1
sigma=ABS(node_flux(j,k))/(node_mass_pre(j,k+1))
sigma2=ABS(node_flux(j,k))/(node_mass_pre(j,k))
width=celldy(k)
vdiffuw=vel1(j,k+1)-vel1(j,k+2)
vdiffdw=vel1(j,k)-vel1(j,k+1)
vdiffuw2=vel1(j,k)-vel1(j,k-1)
vdiffdw2=-vdiffdw
auw=ABS(vdiffuw)
adw=ABS(vdiffdw)
auw2=ABS(vdiffuw2)
wind=1.0_8
wind2=1.0_8
IF(vdiffdw.LE.0.0) wind=-1.0_8
IF(vdiffdw2.LE.0.0) wind2=-1.0_8
limiter=wind*MIN(width*((2.0_8-sigma)*adw/width+(1.0_8+sigma)*auw/celldy(k+1))/6.0_8,auw,adw)
limiter2=wind2*MIN(width*((2.0_8-sigma2)*adw/width+(1.0_8+sigma2)*auw2/celldy(k-1))/6.0_8,auw2,adw)
IF(vdiffuw*vdiffdw.LE.0.0) limiter=0.0
IF(vdiffuw2*vdiffdw2.LE.0.0) limiter2=0.0
IF(node_flux(j,k).LT.0.0)THEN
advec_vel(j,k)=vel1(j,k+1)+(1.0-sigma)*limiter
ELSE
advec_vel(j,k)=vel1(j,k)+(1.0-sigma2)*limiter2
ENDIF
mom_flux(j,k)=advec_vel(j,k)*node_flux(j,k)
ENDDO
ENDDO
!$OMP END DO
ELSE
!$OMP DO PRIVATE(upwind,donor,downwind,dif,sigma,width,limiter,vdiffuw,vdiffdw,auw,adw,wind)
DO k=y_min-1,y_max+1
DO j=x_min,x_max+1
IF(node_flux(j,k).LT.0.0_8)THEN
upwind=k+2
donor=k+1
downwind=k
dif=donor
ELSE
upwind=k-1
donor=k
downwind=k+1
dif=upwind
ENDIF
sigma=ABS(node_flux(j,k))/(node_mass_pre(j,donor))
width=celldy(k)
vdiffuw=vel1(j,donor)-vel1(j,upwind)
vdiffdw=vel1(j,downwind)-vel1(j,donor)
limiter=0.0_8
IF(vdiffuw*vdiffdw.GT.0.0_8)THEN
auw=ABS(vdiffuw)
adw=ABS(vdiffdw)
wind=1.0_8
IF(vdiffdw.LE.0.0_8) wind=-1.0_8
limiter=wind*MIN(width*((2.0_8-sigma)*adw/width+(1.0_8+sigma)*auw/celldy(dif))/6.0_8,auw,adw)
ENDIF
advec_vel(j,k)=vel1(j,donor)+(1.0_8-sigma)*limiter
mom_flux(j,k)=advec_vel(j,k)*node_flux(j,k)
ENDDO
ENDDO
!$OMP END DO
ENDIF
!$OMP DO
DO k=y_min,y_max+1
DO j=x_min,x_max+1
vel1 (j,k)=(vel1(j,k)*node_mass_pre(j,k)+mom_flux(j,k-1)-mom_flux(j,k))/node_mass_post(j,k)
ENDDO
ENDDO
!$OMP END DO
ENDIF
!$OMP END PARALLEL
END SUBROUTINE advec_mom_kernel
END MODULE advec_mom_kernel_mod