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flow_statistics_combine.F90
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flow_statistics_combine.F90
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! C----*|--.---------.---------.---------.---------.---------.---------.-|-------|
SUBROUTINE SAVE_STATS_CURVI(FINAL)
! C----*|--.---------.---------.---------.---------.---------.---------.-|-------|
USE ntypes
USE Domain
USE Grid
USE Fft_var, ONLY : pi
USE TIME_STEP_VAR
USE run_variable
USE variable_stat
USE les_chan_var
USE mpi_var
USE mg_vari, ONLY : INIT_FLAG
implicit none
LOGICAL FINAL, dir_exists
integer i,j,k,n
REAL(r8) ubulk, vbulk, area
REAL(r8) dummy1(0:NZ+1,0:NY+1),dummy2(0:NZ+1,0:NY+1)
REAL(r8) dummy3(0:NZ+1,0:NY+1),dummy4(0:NZ+1,0:NY+1), dummy5(1:NZ+1,1:NY+1)
CHARACTER*29 file_name
CHARACTER*3 PID
CHARACTER*5 file_num
LOGICAL TKE_BUDGET, SAVE_3D, SAVE_SPAN_XY, SAVE_CS, SAVE_SPAN_XZ, HIGH_MOMENT, SAVE_SPAN_ZY
INTEGER, DIMENSION(:), ALLOCATABLE :: seed
! C Initialize the random number generator
CALL RANDOM_SEED(SIZE = K)
Allocate (seed(1:K))
seed(1:K)=10
CALL RANDOM_SEED(PUT = seed)
TKE_BUDGET = .True.
SAVE_3D = .False.
SAVE_SPAN_XY = .TRUE.
SAVE_SPAN_XZ = .TRUE.
SAVE_SPAN_ZY = .TRUE.
SAVE_CS = .FALSE.
HIGH_MOMENT = .FALSE.
IF ( rank .eq. 0) THEN
OPEN(99,file = 'out_screen.txt',form='formatted', status='unknown', position='append')
WRITE(99,*) 'Saving flow statistics.'
WRITE(6,*) 'Saving flow statistics.'
WRITE(6,*) 'Allocate all the tmp arrays'
ENDIF
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! need to allocate temp variables
CALL allocate_temps
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
!
! ! Compute and write out the centerline velocity
! IF (int(float(NY)/2.) .eq. float(NY)/2.) THEN
! ! IF NY is even
! IF (int(float(NZ)/2.) .eq. float(NZ)/2.) THEN
! ! uc=dble(CU3X(0,NZ/2,int(float(NY)/2.)))
! ELSE
! ! uc=0.5*(dble(CU3X(0,int(float(NZ)/2.)-1,NY/2.) &
! ! + CU3X(0,int(float(NZ)/2.),NY/2) ))
! ENDIF
! ELSE
! ! uc=0.5*(dble(CU3X(0,NZ/2,int(float(NY)/2.)-1)) &
! ! +dble(CU3X(0,NZ/2,int(float(NY)/2.))))
! ENDIF
IF (RANK .eq. 0) THEN
! write(*,*) 'Centerline velocity = ', uc
! Compute and write out bulk velocity
! Integrat the instantaneous mean profile numerically at GY points
UBULK=0.0d0
VBULK=0.0d0
DO J=1,NY
DO K=1,NZ
UBULK= UBULK + 0.25d0 * (dble(CU3X(0,K,J))+dble(CU3X(0,K-1,J)) + &
dble(CU3X(0,K-1,J-1)) + dble(CU3X(0,K,J-1)))
VBULK= VBULK + 0.25d0 * (dble(CU1X(0,K,J))+dble(CU1X(0,K-1,J)) + &
dble(CU1X(0,K-1,J-1)) + dble(CU1X(0,K,J-1)))
ENDDO
ENDDO
UBULK = UBULK/real(NY*NZ)
VBULK = VBULK/real(NY*NZ)
! Write out UBULK
WRITE(*,*) 'UBULK: ',UBULK
ENDIF
! Save CUi
DO k=0,NZ+1
DO i=0,NX2P
DO j=0,NY+1
CR1X(i,k,j) = CU1X(i,k,j)
CR2X(i,k,j) = CU2X(i,k,j)
CR3X(i,k,j) = CU3X(i,k,j)
! THIS STEPs ARE REQURIED WHEN DERIVATIVES w.r.t X IS REQURIED LATER
CF1X(i,k,j) = CU1X(i,k,j)
CF2X(i,k,j) = CU2X(i,k,j)
CF3X(i,k,j) = CU3X(i,k,j)
ENDDO
ENDDO
ENDDO
! TRANSFERRING MEAN TO ALL NODES
DO k=1,NZ
DO j=1,NY
p_mean(k,j) = CPX(0,k,j)
ENDDO
ENDDO
CALL MPI_BCAST_REAL(p_mean ,NZ+2, NY+2)
DO k=0,NZ+1
DO j=0,NY+1
dummy1(k,j)=CR1X(0,k,j)
dummy2(k,j)=CR2X(0,k,j)
dummy3(k,j)=CR3X(0,k,j)
ENDDO
ENDDO
CALL MPI_BCAST_REAL(dummy1,NZ+2,NY+2)
CALL MPI_BCAST_REAL(dummy2,NZ+2,NY+2)
CALL MPI_BCAST_REAL(dummy3,NZ+2,NY+2)
DO k=0,NZ+1
DO j=0,NY+1
! IF (W_BC_ZMAX .NE. 6) THEN
CR1X(0,k,j)=dummy1(k,j)
CR2X(0,k,j)=dummy2(k,j)
CR3X(0,k,j)=dummy3(k,j)
! ELSE
! CR1X(0,k,j)=SUM(dummy1(1:NZ,j))/dble(NZ)
! CR2X(0,k,j)=SUM(dummy2(1:NZ,j))/dble(NZ)
! CR3X(0,k,j)=SUM(dummy3(1:NZ,j))/dble(NZ)
! ENDIF
ENDDO
ENDDO
! Computing CS in flow
IF (SAVE_CS) CALL CMP_CS
! Convert to physical space
CALL REAL_FOURIER_TRANS_U1 (.false.)
CALL REAL_FOURIER_TRANS_U2 (.false.)
CALL REAL_FOURIER_TRANS_U3 (.false.)
! pressure has been already convereted back in COMP_CS subrotine
IF (.NOT. SAVE_CS) CALL REAL_FOURIER_TRANS_P (.false.)
! ! Get the turbulent kinetic energy at each level
DO k=0,NZ+1
DO j=0,NY+1
IF (AMP_OMEGA0 .EQ. 0.d0) THEN
TKE(k,j)= ( dble(CR1X(0,k,j)) ** 2.0 + dble(CR2X(0,k,j)) ** 2.0 &
+ dble(CR3X(0,k,j)) ** 2.0)
ELSE
TKE(k,j)= ( dble(CR1X(0,k,j)) ** 2.0 + dble(CR2X(0,k,j)) ** 2.0 &
+ dble(CR3X(0,k,j)) ** 2.0) * dble(AMP_OMEGA0/OMEGA0)**(-2.0)
ENDIF
ENDDO
ENDDO
DO K=0,NZ+1
DO J=0,NY+1
urms(k,j)=0.d0
vrms(k,j)=0.d0
wrms(k,j)=0.d0
DO i=0,min(NXP,NXP_L)
urms(k,j) = urms(k,j) + ( U1X(i,k,j) - dble(CR1X(0,k,j)) ) ** 2.0d0
vrms(k,j) = vrms(k,j) + ( U2X(i,k,j) - dble(CR2X(0,k,j)) ) ** 2.0d0
wrms(k,j) = wrms(k,j) + ( U3X(i,k,j) - dble(CR3X(0,k,j)) ) ** 2.0d0
ENDDO
! urms(k,j)=dsqrt(urms(k,j)/(dble(NX)))
! vrms(k,j)=dsqrt(vrms(k,j)/(dble(NX)))
! wrms(k,j)=dsqrt(wrms(k,j)/(dble(NX)))
ENDDO
ENDDO
! Compute the Reynolds stress and mean velocity gradient
DO k=1,NZ
DO j=0,NY+1
uv(k,j)=0.d0
uw(k,j)=0.d0
wv(k,j)=0.d0
pv(k,j)=0.d0
DO i=0,min(NXP,NXP_L)
uv(k,j) = uv(k,j) + ( U1X(i,k,j) - dble( CR1X(0,k,j)) ) * (U2X(i,k,j) - dble( CR2X(0,k,j) ))
wv(k,j) = wv(k,j) + ( U3X(i,k,j) - dble( CR3X(0,k,j)) ) * (U2X(i,k,j) - dble( CR2X(0,k,j) ))
uw(k,j) = uw(k,j) + ( U1X(i,k,j) - dble( CR1X(0,k,j)) ) * (U3X(i,k,j) - dble( CR3X(0,k,j) ))
pu(k,j) = pu(k,j) + ( U3X(i,k,j) - dble( CR3X(0,k,j)) ) * (PX(i,k,j) - dble( p_mean(k,j) ))
pv(k,j) = pv(k,j) + ( U2X(i,k,j) - dble( CR2X(0,k,j)) ) * (PX(i,k,j) - dble( p_mean(k,j) ))
ENDDO
uv(k,j) = uv(k,j) / float(NX)
uw(k,j) = uw(k,j) / float(NX)
wv(k,j) = wv(k,j) / float(NX)
pu(k,j) = pu(k,j) / float(NX)
pv(k,j) = pv(k,j) / float(NX)
ENDDO
ENDDO
! Get the y-derivative of the mean velocity at GYF points
! do j=1,NY
! dudy(j)=dble(CR1X(0,0,j+1)-CR1X(0,0,j-1))/(2.*DYF(j))
! dwdy(j)=dble(CR3X(0,0,j+1)-CR3X(0,0,j-1))/(2.*DYF(j))
! ENDDO
! Get the y-derivative of the mean velocity at GY points
DO K=ZSTART,ZEND
DO J=JSTART,JEND
dudy(k,j) = ( 0.125 * (CJOB_12(K,J,1) + CJOB_12(K,J+1,1) + CJOB_12(K,J,2) + CJOB_12(K+1,J,2) ) &
* dble ( CR1X(0,k+1,j) - CR1X(0,k-1,j) ) &
+ 0.125 * (CJOB_22(K,J,1) + CJOB_22(K,J+1,1) + CJOB_22(K,J,2) + CJOB_22(K+1,J,2) ) &
* dble ( CR1X(0,k,j+1) - CR1X(0,k,j-1)) )/ INT_JACOB(K,J)
dwdy(k,j) = ( 0.125 * (CJOB_12(K,J,1) + CJOB_12(K,J+1,1) + CJOB_12(K,J,2) + CJOB_12(K+1,J,2) ) &
* dble ( CR3X(0,k+1,j) - CR3X(0,k-1,j) ) &
+ 0.125 * (CJOB_22(K,J,1) + CJOB_22(K,J+1,1) + CJOB_22(K,J,2) + CJOB_22(K+1,J,2) ) &
* dble ( CR3X(0,k,j+1) - CR3X(0,k,j-1)) ) / INT_JACOB(K,J)
ENDDO
ENDDO
DO k=1,NZ
dudy(k,0)=dudy(k,1)
dwdy(k,0)=dwdy(k,1)
dudy(k,NY+1)=dudy(k,NY)
dwdy(k,NY+1)=dwdy(k,NY)
ENDDO
DO k=1,NZ
DO j=1,NY
dudz(k,j) = ( 0.125 * (CJOB_21(K,J,1) + CJOB_21(K,J+1,1) + CJOB_21(K,J,2) + CJOB_21(K+1,J,2) ) &
* dble ( CR1X(0,k,j+1) - CR1X(0,k,j-1) ) &
+ 0.125 * (CJOB_11(K,J,1) + CJOB_11(K,J+1,1) + CJOB_11(K,J,2) + CJOB_11(K+1,J,2) ) &
* dble ( CR1X(0,k+1,j) - CR1X(0,k-1,j)) ) / INT_JACOB(K,J)
dwdz(k,j) = ( 0.125 * (CJOB_21(K,J,1) + CJOB_21(K,J+1,1) + CJOB_21(K,J,2) + CJOB_21(K+1,J,2) ) &
* dble ( CR3X(0,k,j+1) - CR3X(0,k,j-1) ) &
+ 0.125 * (CJOB_11(K,J,1) + CJOB_11(K,J+1,1) + CJOB_11(K,J,2) + CJOB_11(K+1,J,2) ) &
* dble ( CR3X(0,k+1,j) - CR3X(0,k-1,j)) )/ INT_JACOB(K,J)
ENDDO
ENDDO
DO k=1,NZ
dudz(k,0)=dudz(k,1)
dwdz(k,0)=dwdz(k,1)
dudz(k,NY+1)=dudz(k,NY)
dwdz(k,NY+1)=dwdz(k,NY)
ENDDO
DO j=1,NY
dwdz(1,j)=dwdz(2,j)
dudz(1,j)=dudz(2,j)
ENDDO
! Calculate the mean square shear
! DO k=1,NZ
! DO j=1,NY
!
! shear(k,j)=0.d0
!
! DO i=0,min(NXP,NXP_L)
! shear(k,j)=shear(k,j) &
! +( (U1X(i,k,j+1) - U1X(i,k,j-1) ) * (2.d0 * DYF(j)))** (-2.d0) &
! +( (U3X(i,k,j+1) - U3X(i,k,j-1) ) * (2.d0 * DYF(j)))** (-2.d0) &
! +( (U1X(i,k+1,j) - U1X(i,k-1,j) ) * (2.d0 * DZF(k)))** (-2.d0) &
! +( (U3X(i,k+1,j) - U3X(i,k-1,j) ) * (2.d0 * DZF(k)))** (-2.d0)
! ENDDO
! ENDDO
!
! shear(k,j)=shear(k,j) / dble(NX)
! ENDDO
DO k=1,NZ
DO j=1,NY
! omega_x(k,j) = dwdy(k,j) - dudz(k,j)
omega_x(k,j) = ( 0.125 * (CJOB_12(K,J,1) + CJOB_12(K,J+1,1) + CJOB_12(K,J,2)+CJOB_12(K+1,J,2) ) &
* dble ( CR3X(0,k+1,j) - CR3X(0,k-1,j) ) &
+ 0.125 * (CJOB_22(K,J,1) + CJOB_22(K,J+1,1) + CJOB_22(K,J,2)+CJOB_22(K+1,J,2) ) &
* dble ( CR3X(0,k,j+1) - CR3X(0,k,j-1)) ) / INT_JACOB(K,J) &
-( 0.125 * (CJOB_21(K,J,1) + CJOB_21(K,J+1,1) + CJOB_21(K,J,2)+CJOB_21(K+1,J,2) ) &
* dble ( CR2X(0,k,j+1) - CR2X(0,k,j-1) ) &
+ 0.125 * (CJOB_11(K,J,1) + CJOB_11(K,J+1,1) + CJOB_11(K,J,2) + CJOB_11(K+1,J,2) ) &
* dble ( CR2X(0,k+1,j) - CR2X(0,k-1,j)) ) / INT_JACOB(K,J)
! omega_x(k,j)=( (0.5*CJOB_11(K+1,J,2)*(CR2X(0,K,J) +CR2X(0,K+1,J)) &
! - 0.5*CJOB_11(K,J,2)*(CR2X(0,K,J) + CR2X(0,K-1,J))&
! + 0.5*CJOB_21(K,J+1,1)*(CR2X(0,K,J) + CR2X(0,K,J+1))&
! - 0.5*CJOB_21(K,J,1)*(CR2X(0,K,J) + CR2X(0,K,J-1)) )&
! - (0.5*CJOB_12(K+1,J,2)*(CR3X(0,K,J) + CR3X(0,K+1,J))&
! - 0.5*CJOB_12(K,J,2)*(CR3X(0,K,J) + CR3X(0,K-1,J))&
! + 0.5*CJOB_22(K,J+1,1)*(CR3X(0,K,J) + CR3X(0,K,J+1))&
! - 0.5*CJOB_22(K,J,1)*(CR3X(0,K,J) + CR3X(0,K,J-1)) ))/ &
! INT_JACOB(K,J)
ENDDO
ENDDO
DO k=1,NZ
omega_x(k,0) =omega_x(k,1)
omega_x(k,NY+1)=omega_x(k,NY)
ENDDO
! Convert to physical space
! call fft_xz_to_physical(CS1,S1X,0,NY+1)
! Get the rms value
! DO j=1,NY
! omega_x(j)=0.d0
! DO k=1,NZM
! DO i=1,NXP
! omega_x(j)=omega_x(j)+S1X(i,k,j)**2.d0
! ENDDO
! ENDDO
! omega_x(j)=sqrt(omega_x(j)/(dble(NX-1)*dble(NZ-1)))
! ENDDO
! Now, get the y-component in fourier space
! DO j=1,NY
! DO k=0,TNKZ
! DO i=0,NX2P
! CS1(i,k,j)=CIKZ(k)*CR1X(i,k,j)-CIKXP(i)*CR3X(i,k,j)
! ENDDO
! ENDDO
! ENDDO
! Convert to physical space
! call fft_xz_to_physical(CS1,S1X,0,NY+1)
! Get the rms value
! DO j=1,NY
! omega_y(j)=0.d0
! DO k=0,NZM
! DO i=0,NXP
! omega_y(j)=omega_y(j)+S1X(i,k,j)**2.d0
! ENDDO
! ENDDO
! omega_y(j)=sqrt(omega_y(j)/(dble(NX)*dble(NZ)))
! ENDDO
! Now, get the y-component in fourier space
! DO j=1,NY
! DO k=0,TNKZ
! DO i=0,NX2P
! CS1(i,k,j)=CIKXP(i)*0.5d0*(CR2X(i,k,j+1)+CR2X(i,k,j))
! & -(CR1X(i,k,j+1)-CR1X(i,k,j-1))/(2.d0*DYF(j))
! ENDDO
! ENDDO
! CS1(0,0,j)=CS1(0,0,j)-dudy(j)
! ENDDO
! Convert to physical space
! call fft_xz_to_physical(CS1,S1X,0,NY+1)
! Get the rms value
! DO j=1,NY
! omega_z(j)=0.d0
! DO k=0,NZM
! DO i=0,NXP
! omega_z(j)=omega_z(j)+S1X(i,k,j)**2.d0
! ENDDO
! ENDDO
! omega_z(j)=sqrt(omega_z(j)/(dble(NX)*dble(NZ)))
! ENDDO
! Write out the mean statistics at each time as a binary file
IF ( rank .eq. 0) THEN
! check if the folder exists
INQUIRE(DIRECTORY='./plane_data/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'Plane_data directory does not exists'
CALL system('mkdir plane_data')
WRITE(6,*) 'plane_data is created!'
ENDIF
OPEN(66, file='plane_data/time_bulk.txt', form='formatted', status='unknown', position='append' )
WRITE(6,*) TIME_STEP,TIME,DELTA_T
WRITE(66,565) TIME,DELTA_T,UBULK,VBULK,U3X(NXP,2,NY),U1X(NXP,2,NY)
CLOSE(66)
565 format(6f15.7)
WRITE(99,*) TIME_STEP,TIME,DELTA_T
ENDIF
count_data = count_data + 1
! OPEN(60,file='count.txt',form='formatted',status='unknown')
! WRITE(60,*) count_data
! CLOSE(60)
501 format(5(F25.9,' '))
! c call tkebudget_chan_1
! Do over the number of passive scalars
DO N=1,N_TH
! Save CTHX
DO k=0,NZ+1
DO i=0,NX2P
DO j=0,NY+1
CRTHX(i,k,j,n)=CTHX(i,k,j,n)
ENDDO
ENDDO
ENDDO
DO k=0,NZ+1
DO j=0,NY+1
dummy4(k,j)=CRTHX(0,k,j,N)
ENDDO
ENDDO
CALL MPI_BCAST_REAL(dummy4,NZ+2,NY+2)
DO k=0,NZ+1
DO j=0,NY+1
! IF (TH_BC_ZMIN(N) .NE. 6) THEN
CRTHX(0,k,j,N)=dummy4(k,j)
! ELSE
! CRTHX(0,k,j,N)=SUM(dummy4(1:NZ,j))/dble(NZ)
! ENDIF
ENDDO
ENDDO
! Convert to physical space
CALL REAL_FOURIER_TRANS_TH (.false.)
DO j=0,NY+1
DO k=0,NZ+1
thrms(k,j,n)=0.
DO i=0,min(NXP,NXP_L)
thrms(k,j,n) = thrms(k,j,n) + ( abs ( THX(i,k,j,n) -dble(CRTHX(0,k,j,n)) ) )**2.0
ENDDO
! thrms(k,j,n)=sqrt(thrms(k,j,n)/float(NX))
ENDDO
ENDDO
! Get the y-derivative of the mean scalar
! C dt/dy=zeta_y*(T_zeta) + eta_y*(T_eta)
DO k=1,NZ
DO j=1,NY
dthdy(k,j,n) = ( 0.125 * (CJOB_12(K,J,1) + CJOB_12(K,J+1,1) +CJOB_12(K,J,2) + CJOB_12(K+1,J,2) ) &
* dble ( CRTHX(0,k+1,j,n) - CRTHX(0,k-1,j,n)) &
+ 0.125 * (CJOB_22(K,J,1) + CJOB_22(K,J+1,1) +CJOB_22(K,J,2) + CJOB_22(K+1,J,2) ) &
* dble ( CRTHX(0,k,j+1,n) - CRTHX(0,k,j-1,n)) )/ INT_JACOB(K,J)
! adding the background dth/dy
IF (.NOT. CONT_STRAT) THEN
dthdy(k,j,n) = dthdy(k,j,n) + &
( 0.125 * (CJOB_12(K,J,1) + CJOB_12(K,J+1,1) +CJOB_12(K,J,2) + CJOB_12(K+1,J,2) ) &
* ( TH_BAR(k+1,j)-TH_BAR(k-1,j) )&
+ 0.125 * (CJOB_22(K,J,1) + CJOB_22(K,J+1,1) +CJOB_22(K,J,2) + CJOB_22(K+1,J,2) ) &
* ( TH_BAR(k,j+1)-TH_BAR(k,j-1) ) ) / INT_JACOB(K,J)
ENDIF
ENDDO
ENDDO
DO j=1,NY
dthdy(0,j,n) = dthdy(1,j,n)
dthdy(NZ+1,j,n) = dthdy(NZ,j,n)
ENDDO
DO k=0,NZ+1
dthdy(k,0,n) = 2.0 * dthdy(k,1,n)-dthdy(k,2,n)
dthdy(k,NY+1,n) = 2.0 * dthdy(k,NY,n)-dthdy(k,NY-1,n)
ENDDO
! Compute the Reynolds stress and mean velocity gradient
DO j=0,NY+1
DO k=0,NZ+1
thv(k,j,n)=0.0
thw(k,j,n)=0.0
DO i=0,min(NXP,NXP_L)
thv(k,j,n) = thv(k,j,n) + ( THX(i,k,j,n) - dble(CRTHX(0,k,j,n))) * ( U2X(i,k,j) - dble(CR2X(0,k,j)) )
thw(k,j,n) = thw(k,j,n) + ( THX(i,k,j,n) - dble(CRTHX(0,k,j,n))) * ( U3X(i,k,j) - dble(CR3X(0,k,j)) )
ENDDO
thv(k,j,n) = thv(k,j,n) / float(NX)
thw(k,j,n) = thw(k,j,n) / float(NX)
ENDDO
ENDDO
! C dt/dz=zeta_x*(T_zeta) + eta_x*(T_eta)
DO k=1,NZ
DO j=1,NY
dthdz(k,j,n) = ( 0.125 * (CJOB_21(K,J,1) + CJOB_21(K,J+1,1) + CJOB_21(K,J,2) + CJOB_21(K+1,J,2) ) &
* dble ( CRTHX(0,k,j+1,n) - CRTHX(0,k,j-1,n)) &
+ 0.125 * (CJOB_11(K,J,1) + CJOB_11(K,J+1,1) + CJOB_11(K,J,2) + CJOB_11(K+1,J,2) ) &
* dble ( CRTHX(0,k+1,j,n) - CRTHX(0,k-1,j,n)) ) / INT_JACOB(K,J)
ENDDO
ENDDO
DO j=1,NY
dthdz(0,j,n) = dthdz(1,j,n)
dthdz(NZ+1,j,n) = dthdz(NZ,j,n)
ENDDO
DO k=0,NZ+1
dthdz(k,0,n) = 2.0 * dthdz(k,1,n) - dthdz(k,2,n)
dthdz(k,NY+1,n) = 2.0 * dthdz(k,NY,n) - dthdz(k,NY-1,n)
ENDDO
UBULK=0.
DO J=1,NY
DO K=1,NZ
UBULK = UBULK + 0.25 * (dble(CRTHX(0,K,J,n))+dble(CRTHX(0,K-1,J,n)) + &
dble( CRTHX(0,K-1,J-1,n)) + dble(CRTHX(0,K,J-1,n)) )
IF (CONT_STRAT) THEN
IF( dwdy(k,j) .eq. 0.d0 ) THEN
Rig(k,j) = -RI_TAU(N)*(dthdy(k,j,n)-1.d0)*(10.0d8)**2.0
ELSE
Rig(k,j) = -RI_TAU(N)*(dthdy(k,j,n)-1.d0)/ &
(dwdy(k,j)**2.0 + dudy(k,j)**2.0)
ENDIF
ELSE
IF( dwdy(k,j) .eq. 0.d0 ) THEN
Rig(k,j) = -RI_TAU(N)*(dthdy(k,j,n))*(10.0d8)**2.0
ELSE
Rig(k,j) = -RI_TAU(N)*(dthdy(k,j,n))/ &
(dwdy(k,j)**2.0+ dudy(k,j)**2.0)
ENDIF
ENDIF
ENDDO
ENDDO
UBULK = UBULK / real(NY*NZ)
IF (rank .eq. 0) THEN
WRITE(*,*) 'THBULK: ',UBULK, 'Ri', RI_TAU(1)
WRITE(99,*) 'THBULK: ',UBULK, 'Ri', RI_TAU(1)
ENDIF
! ! Compute the potential energy dissipation, grad(THX) \cdot grad(THX)
! c DO j=1,NY
! c pe_diss(j,n)=0.d0
! c DO k=0,NZM
! c DO i=0,NXP
! c pe_diss(j,n)=pe_diss(j,n)
! c & +R1X(i,k,j)**2.d0+R2X(i,k,j)**2.d0+R3X(i,k,j)**2.d0
! c ENDDO
! c ENDDO
! c pe_diss(j,n)=pe_diss(j,n)/dble(NX*NZ)
! c ENDDO
!!!!!!!!!!!!SAVING FULL 3D DATA!!!!!!!!!!!!!!!!!!!!!!!!!!!
IF (SAVE_3D) THEN
! check for directory existence
INQUIRE(DIRECTORY='./plane_3D/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'Plane_3D directory does not exists'
CALL system('mkdir plane_3D')
WRITE(6,*) 'plane_3D is created!'
ENDIF
k = time_step/SAVE_STATS_INT
PID = CHAR(MOD(Rank+1,1000)/100+48) &
//CHAR(MOD(Rank+1,100)/10+48) &
//CHAR(MOD(Rank+1,10)+48)
file_name = 'plane_3D/data_3d_' &
//CHAR(MOD(k,10000)/1000+48) &
//CHAR(MOD(k,1000)/100+48) &
//CHAR(MOD(k,100)/10+48) &
//CHAR(MOD(k,10)+48) // &
'.pln_' &
//PID
IF (RANK.EQ.0) WRITE(6,*) 'start writing in pln format ',file_name
CALL plot_3D(file_name)
ENDIF
!!!!!!!!!!END oF SAVING 3D DATA!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! ! !!!!!!!!!!!!SAVING SPAN-WISE PLANE DATA!!!!!!!!!!!!!!!!!!!!!!!!!!!
IF ( SAVE_SPAN_XY ) THEN
I=1+RANK
PID = CHAR(MOD(I,1000)/100+48) &
//CHAR(MOD(I,100)/10+48) &
//CHAR(MOD(I,10)+48)
k = time_step/SAVE_STATS_INT
file_num = CHAR(MOD(k,10000)/1000+48) &
//CHAR(MOD(k,1000)/100+48) &
//CHAR(MOD(k,100)/10+48) &
//CHAR(MOD(k,10)+48)//'_'
!check for directory existence
INQUIRE(DIRECTORY='./xy_plane/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'xy_plane directory does not exists'
CALL system('mkdir xy_plane')
WRITE(6,*) 'xy_plane is created!'
ENDIF
k = INT((NZ+1)/4) !you can change this deafult
file_name = 'xy_plane/span1_'//file_num//PID//'.pln'
CALL plane_XY_binary(file_name,k)
k = INT((NZ+1)/2) !you can change this deafult
file_name = 'xy_plane/span2_'//file_num//PID//'.pln'
CALL plane_XY_binary(file_name,k)
k = INT(3*(NZ+1)/4) !you can change this deafult
file_name = 'xy_plane/span3_'//file_num//PID//'.pln'
CALL plane_XY_binary(file_name,k)
ENDIF
IF ( SAVE_SPAN_ZY ) THEN
k = time_step/SAVE_STATS_INT
file_num = CHAR(MOD(k,10000)/1000+48) &
//CHAR(MOD(k,1000)/100+48) &
//CHAR(MOD(k,100)/10+48) &
//CHAR(MOD(k,10)+48)//'_'
!check for directory existence
INQUIRE(DIRECTORY='./zy_plane/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'zy_plane directory does not exists'
CALL system('mkdir zy_plane')
WRITE(6,*) 'zy_plane is created!'
ENDIF
!for 1/n'th plane please set rank = INT(NP/(NXP+1)/n) and I
!=MOD(NX/n,NXP+1)
IF (RANK.EQ. INT(NX/(NXP+1)/4) ) THEN
! the defult for NX/4'th ZY plane
k = MOD(NX/4,NXP+1)
file_name = 'zy_plane/span1_'//file_num//'.pln'
CALL plane_ZY_binary(file_name,k)
ENDIF
IF (RANK.EQ. INT(NX/(NXP+1)/2) ) THEN
! the defult for NX/3'th ZY plane
k = MOD(NX/2,NXP+1)
file_name = 'zy_plane/span2_'//file_num//'.pln'
CALL plane_ZY_binary(file_name,k)
ENDIF
IF (RANK.EQ. INT(NX/(NXP+1)/(4/3)) ) THEN
! the defult for NX/3'th ZY plane
k = MOD(4*NX/3,NXP+1)
file_name = 'zy_plane/span3_'//file_num//'.pln'
CALL plane_ZY_binary(file_name,k)
ENDIF
! IF (RANK.EQ.1) THEN
! !Impilicitly telling processor RANK to write the I'th ZY plane
! ! The overal index = I + rank * (NXP+1)
! k = 23
! file_name = 'zy_plane/span1_'//file_num//'.pln'
! CALL plane_ZY_binary(file_name,k)
! ENDIF
!
! IF (RANK.EQ.3) THEN
! !Impilicitly telling processor RANK to write the I'th ZY plane
! ! The overal index = I + rank * (NXP+1)
! k = 21
! file_name = 'zy_plane/span2_'//file_num//'.pln'
! CALL plane_ZY_binary(file_name,k)
! ENDIF
!
! IF (RANK.EQ.5) THEN
! !Impilicitly telling processor RANK to write the I'th ZY plane
! ! The overal index = I + rank * (NXP+1)
! k = 19
! file_name = 'zy_plane/span3_'//file_num//'.pln'
! CALL plane_ZY_binary(file_name,k)
! ENDIF
ENDIF
IF ( SAVE_SPAN_XZ ) THEN
I=1+RANK
PID = CHAR(MOD(I,1000)/100+48) &
//CHAR(MOD(I,100)/10+48) &
//CHAR(MOD(I,10)+48)
k = time_step/SAVE_STATS_INT
file_num = CHAR(MOD(k,10000)/1000+48) &
//CHAR(MOD(k,1000)/100+48) &
//CHAR(MOD(k,100)/10+48) &
//CHAR(MOD(k,10)+48)//'_'
!check for directory existence
INQUIRE(DIRECTORY='./xz_plane/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'xz_plane directory does not exists'
CALL system('mkdir xz_plane')
WRITE(6,*) 'xz_plane is created!'
ENDIF
!Jose_Flat
J = 2 !you can change this deafult
file_name = 'xz_plane/span1_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
file_name = 'xz_plane/span1_combined'//file_num//'.pln'
CALL plane_XZ_combined_binary(file_name,J)
J = 13 !you can change this deafult
file_name = 'xz_plane/span2_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
J = 29 !you can change this deafult
file_name = 'xz_plane/span3_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
J = 44 !you can change this deafult
file_name = 'xz_plane/span4_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
J = 70 !you can change this deafult
file_name = 'xz_plane/span5_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
J = 98 !you can change this deafult
file_name = 'xz_plane/span6_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
J = 109 !you can change this deafult
file_name = 'xz_plane/span7_'//file_num//PID//'.pln'
CALL plane_XZ_binary(file_name,J)
ENDIF
! ! !!!!!!!!!!END oF SAVING SPAN-WISE PLANE DATA!!!!!!!!!!!!!!!!!!!!!
! Convert back to Fourier space
CALL REAL_FOURIER_TRANS_TH (.true.)
!C call FFT_X_TO_FOURIER(THX(0,0,0,n),CTHX(0,0,0,n),0,NY+1,0,NZ+1)
! End do over number of passive scalars, n
ENDDO
CALL MPI_COMBINE_STATS(urms,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(vrms,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(wrms,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(uv,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(uw,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(wv,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(pu,NZ+2,NY+2)
CALL MPI_COMBINE_STATS(pv,NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(dudz,NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(dudy,NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(dwdz,NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(dwdy,NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(omega_x,NZ+2,NY+2)
! Get the bulk rms value
IF (rank .eq. 0) THEN
DO k=0,NZ+1
DO j=0,NY+1
urms(k,j) = dsqrt(urms(k,j) / dble(NX))
vrms(k,j) = dsqrt(vrms(k,j) / dble(NX))
wrms(k,j) = dsqrt(wrms(k,j) / dble(NX))
ENDDO
ENDDO
urms_b = 0.d0
vrms_b = 0.d0
wrms_b = 0.d0
area = 0.d0
DO k=1,NZ
DO j=1,NY
area = area + INT_JACOB(K,J)
urms_b= urms_b + 0.25d0 * ( urms(k,j) + urms(k,j-1) + urms(k-1,j) + urms(k-1,j-1) ) *INT_JACOB(K,J)
vrms_b= vrms_b + 0.25d0 * ( vrms(k,j) + vrms(k,j-1) + vrms(k-1,j) + vrms(k-1,j-1) ) *INT_JACOB(K,J)
wrms_b= wrms_b + 0.25d0 * ( wrms(k,j) + wrms(k,j-1) + wrms(k-1,j) + wrms(k-1,j-1) ) *INT_JACOB(K,J)
ENDDO
ENDDO
urms_b = urms_b / area
vrms_b = vrms_b / area
wrms_b = wrms_b / area
! Write out the bulk rms velocity
WRITE(*,*) '<U_rms_avg>: ',urms_b
WRITE(*,*) '<V_rms_avg>: ',vrms_b
WRITE(*,*) '<W_rms_avg>: ',wrms_b
WRITE(99,*) '<U_rms_avg>: ',urms_b
WRITE(99,*) '<V_rms_avg>: ',vrms_b
WRITE(99,*) '<W_rms_avg>: ',wrms_b
ENDIF
Do n =1,N_th
dummy5(:,:) = thrms(:,:,n)
CALL MPI_COMBINE_STATS(dummy5,NZ+2,NY+2)
thrms(:,:,n) = dummy5(:,:)
dummy5(:,:) = thw(:,:,n)
CALL MPI_COMBINE_STATS(dummy5,NZ+2,NY+2)
thw(:,:,n) = dummy5(:,:)
dummy5(:,:) = thv(:,:,n)
CALL MPI_COMBINE_STATS(dummy5,NZ+2,NY+2)
thv(:,:,n) = dummy5(:,:)
! CALL MPI_COMBINE_STATS(thv(:,:,n),NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(thw(:,:,n),NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(dthdz(0,0,n),NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(dthdy(0,0,n),NZ+2,NY+2)
! CALL MPI_COMBINE_STATS(Rig,NZ+2,NY+2)
IF (rank .eq. 0) THEN
DO j=0,NY+1
DO k=0,NZ+1
thrms(k,j,n) = sqrt( thrms(k,j,n) / float(NX) )
ENDDO
ENDDO
ENDIF
ENDDO
!!!!!!!!!!!!!TKE BUDGET!!!!!!!!!!!!!!!!!!!!!
IF (TKE_BUDGET) THEN
! check for directory existence
INQUIRE(DIRECTORY='./plane_tke/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'Plane_tke directory does not exists'
CALL system('mkdir plane_tke')
WRITE(6,*) 'plane_tke is created!'
ENDIF
CALL tkebudget_curvi_duct
ENDIF
!!!!!!!!!!!!END OF TKE BUDGET!!!!!!!!!!!!!!!
!!!!!!!!!!!!!HIGH MOMEMNTUMS!!!!!!!!!!!!!!!!!!!!!
IF (HIGH_MOMENT) THEN
! check for directory existence
INQUIRE(DIRECTORY='./plane_mmnt/.', EXIST=dir_exists)
IF ( .NOT. dir_exists) THEN
WRITE(6,*) 'Plane_mmnt directory does not exists'
CALL system('mkdir plane_mmnt')
WRITE(6,*) 'plane_mmnt is created!'
ENDIF
CALL high_oder_momentums_curvi
ENDIF
!!!!!!!!!!!!HIGH MOMEMNTUMS!!!!!!!!!!!!!!!
! C Convert velocity back to Fourier space
CALL REAL_FOURIER_TRANS_U1 (.true.)
CALL REAL_FOURIER_TRANS_U2 (.true.)
CALL REAL_FOURIER_TRANS_U3 (.true.)
CALL REAL_FOURIER_TRANS_P (.true.)
CF1X = (0.d0,0.d0)
CF2X = (0.d0,0.d0)
CF3X = (0.d0,0.d0)
!
!C call fft_x_to_fourier(U1X,CU1X,0,NY+1,0,NZ+1)
!C call fft_x_to_fourier(U2X,CU2X,0,NY+1,0,NZ+1)
!C call fft_x_to_fourier(U3X,CU3X,0,NY+1,0,NZ+1)
!C call fft_x_to_fourier(PX,CPX,0,NY+1,0,NZ+1)
! combine all statistics and send to root==rank-0
!VELOCITY FIELD STATISTICS
IF (rank .eq. 0 ) THEN
k = time_step/SAVE_STATS_INT
file_name = 'plane_data/data_tec_' &
//CHAR(MOD(k,100000)/10000+48) &
//CHAR(MOD(k,10000)/1000+48) &
//CHAR(MOD(k,1000)/100+48) &
//CHAR(MOD(k,100)/10+48) &
//CHAR(MOD(k,10)+48) // &
'.pln'
! writing the plane averaged statistics in binary format
CALL plot_binary(file_name)
IF ( WRITE_VEL_TECPLOT ) THEN
file_name = 'plane_data/data_tec_' &
//CHAR(MOD(k,100000)/10000+48) &
//CHAR(MOD(k,10000)/1000+48) &
//CHAR(MOD(k,1000)/100+48) &
//CHAR(MOD(k,100)/10+48) &
//CHAR(MOD(k,10)+48) // &
'.plt'
! writing the plane averaged statistics in tecplot format
CALL plot_tecplot(file_name)
ENDIF
WRITE(99,*) 'done save_stats curvi'
WRITE(*,*) 'done save_stats curvi'
CLOSE(99)
ENDIF
! need to deallocate all the arrays
CALL deallocate_temps
! CCCCCCCCCCCCCCCCCCCCCCCCCC
IF (rank.EQ.0) THEN
WRITE(*,*) 'Dealloc tmp: SAVE_STATS_CURVI'
WRITE(*,*)
WRITE(*,*) 'Saving Stats is Completed!'
ENDIF
IF (FINAL) THEN
WRITE(*,*) 'LAST Saving is done! GOODBYE.'
ENDIF
RETURN
END
!-------------------------------------C---
SUBROUTINE high_oder_momentums_curvi
!-------------------------------------C--
! NOte, it is important to only run this routine after complete R-K
! time advancement since F1 is overwritten which is needed between R-K steps
! This subroutine should be called in SAVE_STATS_CHAN after computing
! plane averaged statistics, with the velocity in physical space, and
! CRi containing the velocity in Fourier space
USE ntypes
USE Domain
USE Grid
USE Fft_var, ONLY : CIKXP
USE TIME_STEP_VAR
USE run_variable
USE mg_vari, ONLY : INIT_FLAG
USE variable_stat
USE mpi_var
IMPLICIT NONE
INTEGER I,J,K,N
CHARACTER*33 file_name
REAL*8 u_prime_tmp(0:NZ+1,0:NY+1), tmp(0:NZ+1,0:NY+1), tmp_1
DO J=0,NY+1
DO K=0,NZ+1
UU(K,J)=0.d0; VV(K,J)=0.d0;
WW(K,J)=0.d0; UUU(K,J)=0.d0;
VVV(K,J)=0.d0; WWW(K,J)=0.d0;
WWV(K,J)=0.d0; UUV(K,J)=0.d0;
UUUU(K,J)=0.d0; VVVV(K,J)=0.d0;
WWWW(K,J)=0.d0; UUUV(K,J)=0.d0;
WWWV(K,J)=0.d0;