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CreateGrid.F90
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CreateGrid.F90
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!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! !
! FILE: CreateGrid.F90 !
! CONTAINS: subroutine CreateGrid !
! !
! PURPOSE: Compute the indices, grid, grid metrics !
! and coefficients for differentiation !
! !
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
subroutine CreateGrid
use param
use AuxiliaryRoutines
implicit none
real :: x1,x2,x3
real :: a33, a33m, a33p
real :: delet, etain, tstr3
real :: z2dp
real, allocatable, dimension(:) :: etaz, etazm
integer :: i, j, kc, km, kp
integer :: nxmo, nclip
do kc=1,nxm
kmv(kc)=kc-1
kpv(kc)=kc+1
if(kc.eq.1) kmv(kc)=kc
if(kc.eq.nxm) kpv(kc)=kc
end do
do kc=1,nxm
kpc(kc)=kpv(kc)-kc
kmc(kc)=kc-kmv(kc)
end do
!
! UNIFORM (HORIZONTAL DIRECTIONS) GRID
!
do i=1,nz
x1=real(i-1)/real(nzm)
zc(i)= zlen*x1
end do
do i=1,nzm
zm(i)=(zc(i)+zc(i+1))*0.5d0
end do
do j=1,ny
x2=real(j-1)/real(nym)
yc(j)= ylen*x2
end do
do j=1,nym
ym(j)=(yc(j)+yc(j+1))*0.5d0
end do
!
! VERTICAL COORDINATE DEFINITION
!
! OPTION 0: UNIFORM CLUSTERING
!
call AllocateReal1DArray(etaz,1,nx+500)
call AllocateReal1DArray(etazm,1,nx+500)
if (istr3.eq.0) then
do kc=1,nx
x3=real(kc-1)/real(nxm)
etaz(kc)=alx3*x3
xc(kc)=etaz(kc)
enddo
endif
!
! OPTION 4: HYPERBOLIC TANGENT-TYPE CLUSTERING
!
tstr3=tanh(str3)
if (istr3.eq.4) then
xc(1)=0.0d0
do kc=2,nx
z2dp=float(2*kc-nx-1)/float(nxm)
xc(kc)=(1+tanh(str3*z2dp)/tstr3)*0.5*alx3
if(xc(kc).lt.0.or.xc(kc).gt.alx3)then
write(*,*)'Grid is too streched: ','zc(',kc,')=',xc(kc)
stop
endif
end do
end if
!
! OPTION 6: CLIPPED CHEBYCHEV-TYPE CLUSTERING
!
if(istr3.eq.6) then
nclip = int(str3)
nxmo = nx+nclip+nclip
do kc=1,nxmo
etazm(kc)=+cos(pi*(float(kc)-0.5)/float(nxmo))
end do
do kc=1,nx
etaz(kc)=etazm(kc+nclip)
end do
delet = etaz(1)-etaz(nx)
etain = etaz(1)
do kc=1,nx
etaz(kc)=etaz(kc)/(0.5*delet)
end do
xc(1) = 0.
do kc=2,nxm
xc(kc) = alx3*(1.-etaz(kc))*0.5
end do
xc(nx) = alx3
endif
call DestroyReal1DArray(etaz)
call DestroyReal1DArray(etazm)
!m-----------------------------------------
!
! METRIC FOR UNIFORM DIRECTIONS
!
dx=real(nxm)/alx3
dy=real(nym)/ylen
dz=real(nzm)/zlen
dxq=dx*dx
dyq=dy*dy
dzq=dz*dz
!
! STAGGERED COORDINATES AND
! METRIC QUANTITIES FOR NON-UNIFORM
! DIRECTIONS
!
do kc=1,nxm
xm(kc)=(xc(kc)+xc(kc+1))*0.5d0
g3rm(kc)=(xc(kc+1)-xc(kc))*dx
enddo
do kc=2,nxm
g3rc(kc)=(xc(kc+1)-xc(kc-1))*dx*0.5d0
enddo
g3rc(1)=(xc(2)-xc(1))*dx
g3rc(nx)= (xc(nx)-xc(nxm))*dx
!
! WRITE GRID INFORMATION
!
do kc=1,nxm
udx3m(kc) = dx/g3rm(kc)
udx3c(kc) = dx/g3rc(kc)
end do
udx3c(nx) = dx/g3rc(nx)
!m====================================================
if(ismaster) then
open(unit=78,file='axicor.out',status='unknown')
do kc=1,nx
write(78,345) kc,xc(kc),xm(kc),g3rc(kc),g3rm(kc)
end do
close(78)
345 format(i4,4(2x,e23.15))
!m===================================================
!
! QUANTITIES FOR DERIVATIVES
!
open(unit=78,file='fact3.out',status='unknown')
do kc=1,nxm
write(78,*) kc,udx3m(kc),udx3c(kc)
end do
write(78,*) nx,udx3m(nxm),udx3c(nx)
close(78)
endif
!
! COEFFICIENTS FOR DIFFERENTIATION FOR NON-UNIFORM GRID
!
! Q3 DIFFERENTIATION (CENTERED VARIABLE)
!
am3ck(1)=0.d0
ap3ck(1)=0.d0
ac3ck(1)=1.d0
am3ck(nx)=0.d0
ap3ck(nx)=0.d0
ac3ck(nx)=1.d0
do kc=2,nxm
km=kc-1
kp=kc+1
a33=dxq/g3rc(kc)
a33p=1.d0/g3rm(kc)
a33m=1.d0/g3rm(km)
ap3ck(kc)=a33*a33p
am3ck(kc)=a33*a33m
ac3ck(kc)=-(ap3ck(kc)+am3ck(kc))
enddo
!
! Q1/Q2 DIFFERENTIATION (STAGGERED VARIABLE)
!
!
do kc=2,nxm-1
kp=kc+1
km=kc-1
a33=dxq/g3rm(kc)
a33p= +a33/g3rc(kp)
a33m= +a33/g3rc(kc)
ap3sk(kc)=a33p
am3sk(kc)=a33m
ac3sk(1,kc)=-(ap3sk(kc)+am3sk(kc))
ac3sk(2,kc)=-(ap3sk(kc)+am3sk(kc))
enddo
!
! LOWER WALL BOUNDARY CONDITIONS (INSLWS SETS NO-SLIP vs STRESS-FREE WALL)
!
kc=1
kp=kc+1
a33=dxq/g3rm(kc)
a33p= +a33/g3rc(kp)
a33m= +a33/g3rc(kc)
ap3sk(kc)=a33p
am3sk(kc)=0.d0
ac3sk(1,kc)=-(a33p+1.0*a33m*2.d0)!no-slip
ac3sk(2,kc)=-(a33p+0.0*a33m*2.d0)!slip
!
! UPPER WALL BOUNDARY CONDITIONS (INSLWN SETS NO-SLIP vs STRESS-FREE WALL)
!
kc=nxm
kp=kc+1
a33=dxq/g3rm(kc)
a33p= +a33/g3rc(kp)
a33m= +a33/g3rc(kc)
am3sk(kc)=a33m
ap3sk(kc)=0.d0
ac3sk(1,kc)=-(a33m+1.0*a33p*2.d0) !no-slip
ac3sk(2,kc)=-(a33m+0.0*a33p*2.d0) !slip
am3ssk(1)=0.d0
ap3ssk(1)=0.d0
ac3ssk(1)=1.d0
!
! TEMPERATURE DIFFERENTIATION (CENTERED VARIABLE)
!
do kc=2,nxm
kp=kc+1
km=kc-1
a33=dxq/g3rc(kc)
a33p=1.d0/g3rm(kc)
a33m=1.d0/g3rm(km)
ap3ssk(kc)=a33*a33p
am3ssk(kc)=a33*a33m
ac3ssk(kc)=-(ap3ssk(kc)+am3ssk(kc))
enddo
am3ssk(nx)=0.d0
ap3ssk(nx)=0.d0
ac3ssk(nx)=1.d0
return
end