TALK=T;RUN(1,1)
PHOTON USE
p
phi
use patgeo
msg Geometry
msg Return to continue
pause
msg Velocity Vectors
msg Return to continue
VECTOR X 1 Z 1 12 Y 1 5 SH DASH 0
VECTOR X 5 Z 1 12 Y 1 5 SH DASH 0
VECTOR Y 1 X 1 5 Z 1 12 SH DASH 0
VECTOR Y 5 X 1 5 Z 1 12 SH DASH 0
VECTOR Z 1 X 1 5 Y 1 5 SH DASH 0
VECTOR Z 12 X 1 5 Y 1 5 SH DASH 0
pause
msg Pressure(P1) Contours
msg Return to continue
CONTOUR P1 X 1 Z 1 12 Y 1 5 FILL; 2.00E-03
CONTOUR P1 X 5 Z 1 12 Y 1 5 FILL; 2.00E-03
CONTOUR P1 Y 1 X 1 5 Z 1 12 FILL; 2.00E-03
CONTOUR P1 Y 5 X 1 5 Z 1 12 FILL; 2.00E-03
CONTOUR P1 Z 1 X 1 5 Y 1 5 FILL; 2.00E-03
CONTOUR P1 Z 12 X 1 5 Y 1 5 FILL; 2.00E-03
msg Press e to END
ENDUSE
DISPLAY
The geometry is that of the B-type impeller tested by Mizuki
et al. (1974), and the calculation is as described in CHAM TR122
(1985) and is for design flow. The solution domain represents the
passage between two blades and a 'vaneless space' beyond the outer
radius of the impeller, which is represented by applying cyclic
boundary conditions on the East and West surfaces at IZ=11 and 12.
The grid given in file GRID1 was generated by linear
interpolation from boundary values using a conical coordinate
system, and is non-orthogonal.
A call to GXBFC from GREX is used to set the inlet boundary
conditions by calculating the relative velocity at inlet and
finding its resolutes on the grid directions. It also sets the
source terms throughout the domain needed to represent the
centrifugal and Coriolis accelerations, calculated in GREX by a
call to subroutine GXROTA.
ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(MIZUKI radial flow impeller: B524)
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 14
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 5
XULAST =1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 5
YVLAST =1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 12
ZWLAST =1.
************************************************************
Group 6. Body-Fitted Coordinates
BFC = T ;NONORT = T
NCRT = -1
RSTGEO = F ;SAVGEO = F
UUP = F ;VUP = F ;WUP = F
NGEOM =CHAM
NAMXYZ =CHAM
ANGMIN =20.
DOMAIN( 1, 6, 1, 6, 1, 13)
* Set fixed sub-domain
FIXDOM( 1, 0, 0, 0, 0, 0, 0)
FIXDOM( 2, 0, 0, 0, 0, 0, 0)
FIXDOM( 3, 0, 0, 0, 0, 0, 0)
FIXDOM( 4, 0, 0, 0, 0, 0, 0)
FIXDOM( 5, 0, 0, 0, 0, 0, 0)
FIXDOM( 6, 0, 0, 0, 0, 0, 0)
FIXDOM( 7, 0, 0, 0, 0, 0, 0)
FIXDOM( 8, 0, 0, 0, 0, 0, 0)
FIXDOM( 9, 0, 0, 0, 0, 0, 0)
FIXDOM( 10, 0, 0, 0, 0, 0, 0)
LIJ = F ;LJK = T ;LIK = F
* X-cyclic boundaries switched
XCYIZ( 11, T ) ; XCYIZ( 12, T )
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(1)=P1 ;NAME(3)=U1
NAME(5)=V1 ;NAME(7)=W1
NAME(148)=WCRT ;NAME(149)=VCRT
NAME(150)=UCRT
* Y in SOLUTN argument list denotes:
* 1-stored 2-solved 3-whole-field
* 4-point-by-point 5-explicit 6-harmonic averaging
SOLUTN(P1,Y,Y,Y,N,N,N)
SOLUTN(U1,Y,Y,N,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,Y)
SOLUTN(W1,Y,Y,N,N,N,Y)
SOLUTN(WCRT,Y,N,N,N,N,N)
SOLUTN(VCRT,Y,N,N,N,N,N)
SOLUTN(UCRT,Y,N,N,N,N,N)
************************************************************
Group 8. Terms & Devices
* Y in TERMS argument list denotes:
* 1-built-in source 2-convection 3-diffusion 4-transient
* 5-first phase variable 6-interphase transport
TERMS(P1,Y,Y,Y,N,Y,Y)
TERMS(U1,Y,Y,Y,Y,Y,Y)
TERMS(V1,Y,Y,Y,Y,Y,Y)
TERMS(W1,Y,Y,Y,Y,Y,Y)
DIFCUT =0.5 ;ZDIFAC =1.
GALA = F ;ADDDIF = F
ISOLX = 1 ;ISOLY = 1 ;ISOLZ = 1
************************************************************
Group 9. Properties used if PRPS is not
stored, and where PRPS = -1.0 if it is!
RHO1 =1.24 ;TMP1 =0. ;EL1 =0.
TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
DVO1DT =0. ;DRH1DP =0.
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
ENUL =1.451613E-05 ;ENUT =1.032258E-03
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRNDTL(W1)=1.
PRT(U1)=1. ;PRT(V1)=1.
PRT(W1)=1.
CP1 =1. ;CP2 =1.
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(P1)=1.0E-10 ;FIINIT(U1)=1.0E-10
FIINIT(V1)=1.0E-10 ;FIINIT(W1)=33.929176
FIINIT(WCRT)=1.0E-10 ;FIINIT(VCRT)=1.0E-10
FIINIT(UCRT)=1.0E-10
No PATCHes yet used for this Group
INIADD = F
FSWEEP = 1
NAMFI =CHAM
************************************************************
Group 12. Patchwise adjustment of terms
Patches for this group are printed with those
for Group 13.
Their names begin either with GP12 or &
************************************************************
Group 13. Boundary & Special Sources
PATCH(BFC1 ,LOW , 1, 5, 5, 5, 1, 1, 1, 1)
COVAL(BFC1 ,P1 , FIXFLU ,42.072178 )
COVAL(BFC1 ,U1 ,0. , GRND1 )
COVAL(BFC1 ,V1 ,0. , GRND1 )
COVAL(BFC1 ,W1 ,0. , GRND1 )
COVAL(BFC1 ,WCRT,0. ,33.929176 )
COVAL(BFC1 ,VCRT,0. ,-27.83449 )
COVAL(BFC1 ,UCRT,0. ,0. )
PATCH(BFC2 ,LOW , 1, 5, 4, 4, 1, 1, 1, 1)
COVAL(BFC2 ,P1 , FIXFLU ,42.072178 )
COVAL(BFC2 ,U1 ,0. , GRND1 )
COVAL(BFC2 ,V1 ,0. , GRND1 )
COVAL(BFC2 ,W1 ,0. , GRND1 )
COVAL(BFC2 ,WCRT,0. ,33.929176 )
COVAL(BFC2 ,VCRT,0. ,-32.609707 )
COVAL(BFC2 ,UCRT,0. ,0. )
PATCH(BFC3 ,LOW , 1, 5, 3, 3, 1, 1, 1, 1)
COVAL(BFC3 ,P1 , FIXFLU ,42.072178 )
COVAL(BFC3 ,U1 ,0. , GRND1 )
COVAL(BFC3 ,V1 ,0. , GRND1 )
COVAL(BFC3 ,W1 ,0. , GRND1 )
COVAL(BFC3 ,WCRT,0. ,33.929176 )
COVAL(BFC3 ,VCRT,0. ,-37.384926 )
COVAL(BFC3 ,UCRT,0. ,0. )
PATCH(BFC4 ,LOW , 1, 5, 2, 2, 1, 1, 1, 1)
COVAL(BFC4 ,P1 , FIXFLU ,42.072178 )
COVAL(BFC4 ,U1 ,0. , GRND1 )
COVAL(BFC4 ,V1 ,0. , GRND1 )
COVAL(BFC4 ,W1 ,0. , GRND1 )
COVAL(BFC4 ,WCRT,0. ,33.929176 )
COVAL(BFC4 ,VCRT,0. ,-42.160145 )
COVAL(BFC4 ,UCRT,0. ,0. )
PATCH(BFC5 ,LOW , 1, 5, 1, 1, 1, 1, 1, 1)
COVAL(BFC5 ,P1 , FIXFLU ,42.072178 )
COVAL(BFC5 ,U1 ,0. , GRND1 )
COVAL(BFC5 ,V1 ,0. , GRND1 )
COVAL(BFC5 ,W1 ,0. , GRND1 )
COVAL(BFC5 ,WCRT,0. ,33.929176 )
COVAL(BFC5 ,VCRT,0. ,-46.935356 )
COVAL(BFC5 ,UCRT,0. ,0. )
PATCH(OUTLET ,HIGH , 1, 5, 1, 5, 12, 12, 1, 1)
COVAL(OUTLET ,P1 ,100. ,0. )
COVAL(OUTLET ,U1 ,0. ,0. )
COVAL(OUTLET ,V1 ,0. ,0. )
COVAL(OUTLET ,W1 ,0. ,0. )
PATCH(ROTA ,PHASEM, 1, 5, 1, 5, 1, 12, 1, 1)
COVAL(ROTA ,U1 , FIXFLU , GRND1 )
COVAL(ROTA ,V1 , FIXFLU , GRND1 )
COVAL(ROTA ,W1 , FIXFLU , GRND1 )
PATCH(WFUN1 ,SWALL , 1, 5, 1, 1, 1, 12, 1, 1)
COVAL(WFUN1 ,U1 , GRND2 ,-67.858353 )
COVAL(WFUN1 ,W1 , GRND2 ,0. )
PATCH(WFUN2 ,NWALL , 1, 5, 5, 5, 1, 12, 1, 1)
COVAL(WFUN2 ,U1 , GRND2 ,0. )
COVAL(WFUN2 ,W1 , GRND2 ,0. )
PATCH(WFUN3 ,WWALL , 1, 1, 1, 5, 1, 10, 1, 1)
COVAL(WFUN3 ,V1 , GRND2 ,0. )
COVAL(WFUN3 ,W1 , GRND2 ,0. )
PATCH(WFUN4 ,EWALL , 5, 5, 1, 5, 1, 10, 1, 1)
COVAL(WFUN4 ,V1 , GRND2 ,0. )
COVAL(WFUN4 ,W1 , GRND2 ,0. )
XCYCLE = T
EGWF = T
WALLCO = GRND2
BFCA =1.24
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 200 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =0.1
************************************************************
Group 16. Terminate Iterations
LITER(P1)=10 ;LITER(U1)=1
LITER(V1)=1 ;LITER(W1)=1
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03 ;ENDIT(W1)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,0.4)
RELAX(U1,FALSDT,5.0E-04)
RELAX(V1,FALSDT,5.0E-04)
RELAX(W1,FALSDT,5.0E-04)
RELAX(WCRT,LINRLX,1.)
RELAX(VCRT,LINRLX,1.)
RELAX(UCRT,LINRLX,1.)
OVRRLX =0.
EXPERT = F ;NNORSL = F
************************************************************
Group 18. Limits
VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
VARMAX(U1)=1.0E+06 ;VARMIN(U1)=-1.0E+06
VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
VARMAX(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
VARMAX(WCRT)=1.0E+10 ;VARMIN(WCRT)=-1.0E+10
VARMAX(VCRT)=1.0E+10 ;VARMIN(VCRT)=-1.0E+10
VARMAX(UCRT)=1.0E+10 ;VARMIN(UCRT)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
PARSOL = F
ISG62 = 1
ANGVEL =628.318054
ROTAZB =-1.
SPEDAT(SET,GXMONI,PLOTALL,L,T)
************************************************************
Group 20. Preliminary Printout
************************************************************
Group 21. Print-out of Variables
INIFLD = F ;SUBWGR = F
* Y in OUTPUT argument list denotes:
* 1-field 2-correction-eq. monitor 3-selective dumping
* 4-whole-field residual 5-spot-value table 6-residual table
OUTPUT(P1,Y,Y,Y,Y,Y,Y)
OUTPUT(U1,Y,N,Y,Y,Y,Y)
OUTPUT(V1,Y,N,Y,Y,Y,Y)
OUTPUT(W1,Y,N,Y,Y,Y,Y)
OUTPUT(WCRT,Y,N,Y,N,N,N)
OUTPUT(VCRT,Y,N,Y,N,N,N)
OUTPUT(UCRT,Y,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 2 ;IYMON = 2 ;IZMON = 6
NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
UWATCH = T ;USTEER = T
HIGHLO = F
************************************************************
Group 23.Field Print-Out & Plot Control
NPRINT = 200 ;NUMCLS = 5
NXPRIN = 2 ;IXPRF = 1 ;IXPRL = 10000
NYPRIN = 2 ;IYPRF = 1 ;IYPRL = 10000
NZPRIN = 2 ;IZPRF = 1 ;IZPRL = 10000
XZPR = F ;YZPR = F
IPLTF = 1 ;IPLTL = -1 ;NPLT = 1
ISWPRF = 1 ;ISWPRL = 100000
ITABL = 3 ;IPROF = 1
ABSIZ =0.5 ;ORSIZ =0.4
NTZPRF = 1 ;NCOLPF = 50
ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
PATCH(SUCTION ,CONTUR, 5, 5, 1, 5, 1, 12, 1, 1)
PLOT(SUCTION ,P1 ,0. ,20. )
PATCH(PRESSURE,CONTUR, 1, 1, 1, 5, 1, 12, 1, 1)
PLOT(PRESSURE,P1 ,0. ,20. )
PATCH(MIDWAY ,CONTUR, 1, 5, 2, 2, 1, 12, 1, 1)
PLOT(MIDWAY ,P1 ,0. ,20. )
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP