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|
*DECK THMAVG
SUBROUTINE THMAVG(IPMAP,IMPX,NX,NY,NZ,NCH,TCOMB,TSURF,DCOOL,
> TCOOL,PCOOL,HCOOL,POW,NSIMS)
*
*-----------------------------------------------------------------------
*
*Purpose:
* Print averaged thermalhydraulics properties over the core map.
*
*Copyright:
* Copyright (C) 2012 Ecole Polytechnique de Montreal.
*
*Author(s):
* M. Cordiez
*
*Parameters: input
* IPMAP pointer to the fuelmap object.
* IMPX printing index (=0 for no print).
* NX number of meshes along X direction.
* NY number of meshes along Y direction.
* NZ number of meshes along Z direction (channel direction).
* NCH number of fuel channels in the axial plane.
* TCOMB averaged fuel temperature distribution in K.
* TSURF surface fuel temperature distribution in K.
* DCOOL coolant density distribution in g/cc.
* TCOOL coolant temperature distribution in K.
* PCOOL coolant pressure distribution in Pa.
* HCOOL coolant enthalpty distribution in J/kg.
* POW power distribution in W.
* NSIMS flag greater than zero to activate axial averaging of
* thermohydraulics information.
*
*-----------------------------------------------------------------------
*
USE GANLIB
*----
* SUBROUTINE ARGUMENTS
*----
INTEGER MAXHHX
PARAMETER(MAXHHX=30)
TYPE(C_PTR) IPMAP
INTEGER IMPX,NX,NY,NZ,NCH,NSIMS
REAL TCOMB(NZ,NX,NY),TSURF(NZ,NX,NY),DCOOL(NZ,NX,NY),
> TCOOL(NZ,NX,NY),PCOOL(NZ,NX,NY),HCOOL(NZ,NX,NY),POW(NZ,NX,NY)
*----
* LOCAL VARIABLES
*----
* Variables for an averaged fuel bundle
INTEGER NBLEVELCOMB,IHY(MAXHHX)
REAL TCOMBAVGAVG, TSURFAVGAVG, DCOOLAVGAVG, TCOOLAVGAVG,
> PCOOLAVGAVG, HCOOLAVGAVG, POWAVGAVG, POWRELAVGAVG
REAL TCOMBAVG(NZ), TSURFAVG(NZ), DCOOLAVG(NZ), TCOOLAVG(NZ),
> PCOOLAVG(NZ), HCOOLAVG(NZ), POWERAVG(NZ), POWRELAVG(NZ)
* --> POWRELAVG : relative power by axial plane
* Variables for axially averaged to draw a core map
REAL TCOMBCM(NX,NY),TSURFCM(NX,NY),DCOOLCM(NX,NY),TCOOLCM(NX,NY),
> PCOOLCM(NX,NY),HCOOLCM(NX,NY),POWERCM(NX,NY),POWRELCM(NX,NY)
REAL POWAVGCM, POWRELAVGCM
CHARACTER HHX(MAXHHX)*1,TEXT1*1,TEXT1B*1,TEXT4*4
*----
* ALLOCATABLE ARRAYS
*----
CHARACTER(LEN=4), ALLOCATABLE, DIMENSION(:) :: HZONE
*----
* RECOVER NAVAL BATTLE COORDINATES OF THE MAP
*----
IF(NSIMS.GT.0) THEN
LX=NSIMS/100
LY=MOD(NSIMS,100)
ALLOCATE(HZONE(NCH))
CALL LCMGTC(IPMAP,'S-ZONE',4,NCH,HZONE)
TEXT4=HZONE(1)
READ(TEXT4,'(A1,I2)') TEXT1,INTG2
L=0
DO K=1,NCH
TEXT4=HZONE(K)
READ(TEXT4,'(A1,I2)') TEXT1B,INTG2B
IF(TEXT1B.EQ.TEXT1) THEN
L=L+1
IF(L.GT.MAXHHX)CALL XABORT('@THMAVG: MAXHHX OVERFLOW.(1)')
IF(L.GT.LY)CALL XABORT('@THMAVG: INCOHERENCE IN BASIC '
> //'ASSEMBLY LAYOUT GIVEN IN RESINI: (1).')
IHY(L)=INTG2B
ENDIF
ENDDO
L=L+1
IF(L.GT.MAXHHX)CALL XABORT('@THMAVG: MAXHHX OVERFLOW.(2)')
IHY(L)=0
L=0
DO K=1,NCH
TEXT4=HZONE(K)
READ(TEXT4,'(A1,I2)') TEXT1B,INTG2B
IF(INTG2B.EQ.IHY((LY+1)/2)) THEN
L=L+1
IF(L.GT.MAXHHX)CALL XABORT('@THMAVG: MAXHHX OVERFLOW.(3)')
IF(L.GT.LX)CALL XABORT('@THMAVG: INCOHERENCE IN BASIC '
> //'ASSEMBLY LAYOUT GIVEN IN RESINI: (2).')
HHX(L)=TEXT1B
ENDIF
ENDDO
DEALLOCATE(HZONE)
ENDIF
*----
* VARIABLES INITIALIZATION
*----
* Variables for an average fuel bundle
TCOMBAVGAVG = 0
TSURFAVGAVG = 0
DCOOLAVGAVG = 0
TCOOLAVGAVG = 0
PCOOLAVGAVG = 0
HCOOLAVGAVG = 0
POWAVGAVG = 0
POWRELAVGAVG = 0
NBLEVELCOMB = 0
DO L=1,NZ
TCOMBAVG(L) = 0.0
TSURFAVG(L) = 0.0
DCOOLAVG(L) = 0.0
TCOOLAVG(L) = 0.0
PCOOLAVG(L) = 0.0
HCOOLAVG(L) = 0.0
POWERAVG(L) = 0.0
POWRELAVG(L) = 0.0
ENDDO
* Variables for an averaged core layer (map of values)
POWAVGCM = 0
POWRELAVGCM = 0
*----
* SUM THE VALUES FOR A EVERY FUEL BUNDLE TO AVERAGE THEM
*----
NBASS=0
DO 95 I=1,NX
DO 90 J=1,NY
TCOMBCM(I,J) = 0.0
TSURFCM(I,J) = 0.0
DCOOLCM(I,J) = 0.0
TCOOLCM(I,J) = 0.0
PCOOLCM(I,J) = 0.0
HCOOLCM(I,J) = 0.0
POWERCM(I,J) = 0.0
POWRELCM(I,J) = 0.0
IF(POW((NZ+1)/2,I,J).GT.0.0) THEN
* We do not average on the reflectors whose values equal 0
NBASS=NBASS+1
TCOMBAVG=TCOMBAVG+TCOMB(:,I,J)
TSURFAVG=TSURFAVG+TSURF(:,I,J)
DCOOLAVG=DCOOLAVG+DCOOL(:,I,J)
TCOOLAVG=TCOOLAVG+TCOOL(:,I,J)
PCOOLAVG=PCOOLAVG+PCOOL(:,I,J)
HCOOLAVG=HCOOLAVG+HCOOL(:,I,J)
POWERAVG=POWERAVG+POW(:,I,J)
ENDIF
90 CONTINUE
95 CONTINUE
*----
* COMPUTE THE AVERAGED VALUES FOR A GENERIC FUEL BUNDLE
*----
IF(NSIMS.GT.0) THEN
TCOMBAVG=TCOMBAVG/REAL(NBASS)
TSURFAVG=TSURFAVG/REAL(NBASS)
DCOOLAVG=DCOOLAVG/REAL(NBASS)
TCOOLAVG=TCOOLAVG/REAL(NBASS)
PCOOLAVG=PCOOLAVG/REAL(NBASS)
HCOOLAVG=HCOOLAVG/REAL(NBASS)
POWERAVG=POWERAVG/REAL(NBASS)
*
* Computation of the relative power by axial plane and
* computation of the averaged-on-z-axis values of an average
* fuel bundle
DO L=1,NZ
TCOMBAVGAVG=TCOMBAVGAVG+TCOMBAVG(L)
TSURFAVGAVG=TSURFAVGAVG+TSURFAVG(L)
DCOOLAVGAVG=DCOOLAVGAVG+DCOOLAVG(L)
TCOOLAVGAVG=TCOOLAVGAVG+TCOOLAVG(L)
PCOOLAVGAVG=PCOOLAVGAVG+PCOOLAVG(L)
HCOOLAVGAVG=HCOOLAVGAVG+HCOOLAVG(L)
POWAVGAVG=POWAVGAVG+POWERAVG(L)
IF(POWERAVG(L).NE.0) NBLEVELCOMB=NBLEVELCOMB+1
ENDDO
TCOMBAVGAVG=TCOMBAVGAVG/REAL(NBLEVELCOMB)
TSURFAVGAVG=TSURFAVGAVG/REAL(NBLEVELCOMB)
DCOOLAVGAVG=DCOOLAVGAVG/REAL(NBLEVELCOMB)
TCOOLAVGAVG=TCOOLAVGAVG/REAL(NBLEVELCOMB)
PCOOLAVGAVG=PCOOLAVGAVG/REAL(NBLEVELCOMB)
HCOOLAVGAVG=HCOOLAVGAVG/REAL(NBLEVELCOMB)
POWAVGAVG=POWAVGAVG/REAL(NBLEVELCOMB)
POWRELAVG=POWERAVG/POWAVGAVG
*
* Computation of the average relative power by axial plane
* (it must be equal to 1)
DO L=1,NZ
POWRELAVGAVG=POWRELAVGAVG+POWRELAVG(L)
ENDDO
POWRELAVGAVG=POWRELAVGAVG/REAL(NBLEVELCOMB)
*
* There is no use in computing them if the user does not want them
IF(IMPX.GT.2) THEN
WRITE(6,'(/28H THMAVG: AVERAGE FUEL BUNDLE/1X,27(1H-))')
WRITE(6,210) ' ___________________________________________',
> '_____________________________________________________',
> '___________________'
WRITE(6,210) '| | TFUEL | TSURF | DCOOL ',
> ' | TCOOL | PCOOL | HCOOL | ',
> 'POWER | POW REL |'
WRITE(6,230) '| AVG |',TCOMBAVGAVG,' |',TSURFAVGAVG,' |',
> DCOOLAVGAVG,' |',TCOOLAVGAVG,' |',PCOOLAVGAVG,' |',
> HCOOLAVGAVG,' |',POWAVGAVG,' |',POWRELAVGAVG,' |'
WRITE(6,210) '|_____|_____________|_____________|__________',
> '___|_____________|_____________|_____________|_______',
> '______|___________|'
DO L=NZ,1,-1
IF(L.EQ.1) THEN
WRITE(6,230) '| BOT |',TCOMBAVG(L),' |',TSURFAVG(L),
> ' |',DCOOLAVG(L),' |',TCOOLAVG(L),' |',PCOOLAVG(L),
> ' |',HCOOLAVG(L),' |',POWERAVG(L),' |',
> POWRELAVG(L),' |'
ELSEIF(L.EQ.NZ) THEN
WRITE(6,230) '| TOP |',TCOMBAVG(L),' |',TSURFAVG(L),
> ' |',DCOOLAVG(L),' |',TCOOLAVG(L),' |',PCOOLAVG(L),
> ' |',HCOOLAVG(L),' |',POWERAVG(L),' |',
> POWRELAVG(L),' |'
ELSE
WRITE(6,235) '| ',L,' |',TCOMBAVG(L),' |',TSURFAVG(L),
> ' |',DCOOLAVG(L),' |',TCOOLAVG(L),' |',PCOOLAVG(L),
> ' |',HCOOLAVG(L),' |',POWERAVG(L),' |',
> POWRELAVG(L),' |'
ENDIF
ENDDO
WRITE(6,210) '|_____|_____________|_____________|_________',
> '____|_____________|_____________|_____________|______',
> '_______|___________|'
ENDIF
*----
* COMPUTE THE AVERAGED VALUES ON THE CORE MAP
*----
* We do not average on the reflectors whose values equal 0
DO K=1,NZ
TCOMBCM(:,:)=TCOMBCM(:,:)+TCOMB(K,:,:)
TSURFCM(:,:)=TSURFCM(:,:)+TSURF(K,:,:)
DCOOLCM(:,:)=DCOOLCM(:,:)+DCOOL(K,:,:)
TCOOLCM(:,:)=TCOOLCM(:,:)+TCOOL(K,:,:)
PCOOLCM(:,:)=PCOOLCM(:,:)+PCOOL(K,:,:)
HCOOLCM(:,:)=HCOOLCM(:,:)+HCOOL(K,:,:)
POWERCM(:,:)=POWERCM(:,:)+POW(K,:,:)
ENDDO
TCOMBCM=TCOMBCM/REAL(NBLEVELCOMB)
TSURFCM=TSURFCM/REAL(NBLEVELCOMB)
DCOOLCM=DCOOLCM/REAL(NBLEVELCOMB)
TCOOLCM=TCOOLCM/REAL(NBLEVELCOMB)
PCOOLCM=PCOOLCM/REAL(NBLEVELCOMB)
HCOOLCM=HCOOLCM/REAL(NBLEVELCOMB)
POWERCM=POWERCM/REAL(NBLEVELCOMB)
* Calculation of the relative power distribution (avg = 1)
DO 106 I=1,NX
DO 105 J=1,NY
POWAVGCM=POWAVGCM+POWERCM(I,J)
105 CONTINUE
106 CONTINUE
POWAVGCM=POWAVGCM/REAL(NBASS)
POWRELCM=POWERCM/POWAVGCM
DO 108 I=1,NX
DO 107 J=1,NY
POWRELAVGCM=POWRELAVGCM+POWRELCM(I,J)
107 CONTINUE
108 CONTINUE
POWRELAVGCM=POWRELAVGCM/REAL(NBASS)
*
* There is no use in computing them if the user does not want them
IF(IMPX.GT.2) THEN
IDEB=1
JDEB=1
* We do not draw the reflector
I=1
DO WHILE (POW((NZ+1)/2,I,(NY+1)/2).EQ.0)
IDEB=IDEB+1
I=I+1
END DO
J=1
DO WHILE (POW((NZ+1)/2,(NX+1)/2,J).EQ.0)
JDEB=JDEB+1
J=J+1
END DO
* ********************
* We write the results
* ********************
* Fuel temperature
WRITE(6,'(/25H THMAVG: AVERAGE CORE MAP/1X,24(1H-))')
WRITE(6,202) 'TCOMB'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 111 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 110 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,205,ADVANCE='NO') TCOMBCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
110 CONTINUE
111 CONTINUE
* Surface temperature
WRITE(6,202) 'TSURF'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 113 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 112 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,205,ADVANCE='NO') TSURFCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
112 CONTINUE
113 CONTINUE
* Coolant density
WRITE(6,202) 'DCOOL'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 115 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 114 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,206,ADVANCE='NO') DCOOLCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
114 CONTINUE
115 CONTINUE
* Coolant temperature
WRITE(6,202) 'TCOOL'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 117 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 116 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,205,ADVANCE='NO') TCOOLCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
116 CONTINUE
117 CONTINUE
* Coolant pressure
WRITE(6,202) 'PCOOL'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 119 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 118 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,207,ADVANCE='NO') PCOOLCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
118 CONTINUE
119 CONTINUE
* Coolant enthalpy
WRITE(6,202) 'HCOOL'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 121 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 120 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,207,ADVANCE='NO') HCOOLCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
120 CONTINUE
121 CONTINUE
* Power
WRITE(6,202) 'POWER'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 123 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 122 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,207,ADVANCE='NO') POWERCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
122 CONTINUE
123 CONTINUE
* Power
WRITE(6,209) 'RELATIVE POWER, REFLECTORS EXCLUDED (AVG:',
1 POWRELAVGCM,')'
WRITE(6,203,ADVANCE='NO') (HHX(I),I=1,NX-2*IDEB+2)
DO 125 J=JDEB,NY
WRITE(6,204,ADVANCE='NO') IHY(J-JDEB+1)
ENDLINE=0
DO 124 I=IDEB,NX
IF(POW((NZ+1)/2,I,J).GT.0) THEN
WRITE(6,206,ADVANCE='NO') POWRELCM(I,J)
ENDLINE=1
ELSE IF(ENDLINE.EQ.0) THEN
WRITE(6,208,ADVANCE='NO')
ENDIF
124 CONTINUE
125 CONTINUE
ENDIF
ENDIF
RETURN
*
202 FORMAT(/1X,A)
203 FORMAT(1X,20(8X,1A1))
204 FORMAT(/1X,I2)
205 FORMAT(F9.1)
206 FORMAT(F9.3)
207 FORMAT(1P,E9.2)
208 FORMAT(9X)
209 FORMAT(/1X,A,F7.4,A)
210 FORMAT(1X,A,A,A,A)
230 FORMAT(1X,A,F12.2,A,F12.2,A,F12.4,A,F12.2,A,3P,E12.4,
> A,1P,E12.4,A,1P,E12.4,A,0P,F10.4,A)
235 FORMAT(1X,A,I3,A,F12.2,A,F12.2,A,F12.4,A,F12.2,A,3P,E12.4,
> A,1P,E12.4,A,1P,E12.4,A,0P,F10.4,A)
END
|
