TALK=F;RUN( 1, 1) ************************************************************ Q1 created by VDI menu, Version 2007, Date 26/09/07 CPVNAM=VDI;SPPNAM=Core ************************************************************ Echo DISPLAY / USE settings DISPLAY A rectangular plate with a centrally-placed CIRCULAR hole is extended by uniform equal forces on its left and right surfaces, which are allowed to distort. By reason of symmetry, only one quarter of the plate is analysed. Comparison - a analytical solution (Timoshenko and Goodier). See also: I. Demirdzic, S. Musafija "Finite Volume method for stress analysis in Complex Domains" Int. J. for numerical methods in engineering", v. 37, 3751-3756 (1994).) ENDDIS ************************************************************ IRUNN = 1 ;LIBREF = 202 ************************************************************ Group 1. Run Title TEXT(USP:2D xy Plate with CIRCULAR hole ) ************************************************************ Group 2. Transience STEADY = T ************************************************************ Groups 3, 4, 5 Grid Information * Overall number of cells, RSET(M,NX,NY,NZ,tolerance) RSET(M,10,10,1,1.000000E-05) ************************************************************ Group 6. Body-Fitted coordinates ************************************************************ Group 7. Variables: STOREd,SOLVEd,NAMEd ONEPHS = T * Non-default variable names NAME(133) =XY/T ; NAME(134) =SXYT NAME(135) =SY/T ; NAME(136) =SYTH NAME(137) =SX/T ; NAME(138) =SXTH NAME(139) =TET7 ; NAME(140) =R7 NAME(141) =EPSZ ; NAME(142) =EPSX NAME(143) =EPSY ; NAME(144) =STXY NAME(145) =STRZ ; NAME(146) =STRY NAME(147) =STRX ; NAME(148) =PRPS NAME(149) =DISX ; NAME(150) =DISY * Solved variables list SOLVE(DISX,DISY) * Stored variables list STORE(PRPS,STRX,STRY,STRZ,STXY,EPSY,EPSX,EPSZ) STORE(R7 ,TET7,SXTH,SX/T,SYTH,SY/T,SXYT,XY/T) STORE(ZZZ7) ************************************************************ Echo save-block settings for Group 7 SAVE7BEGIN REAL(FX,LX,LY,R0,POISSON,YOUNG) FX= 1.0e4 LX=2.0 LY=LX R0=0.5 YOUNG = 1/1.0E-7 ! Young's modulus POISSON=0.3 ! Poisson's ratio char(form1,form2) (STORED VAR R7 IS SQRT(XG^2+YG^2)) (STORED VAR TET7 IS ATAN(YG/(XG+1.e-10))) form1=:FX:*(1.0-(:R0:/R7)^2*(1.5*COS(2*TET7)+ form2=COS(4*TET7))+1.50*(:R0:/R7)^4*COS(4*TET7)) (STORED VAR SXTH IS :form1::form2: with imat>100) (STORED VAR SX/T IS STRX/SXTH with imat>100) char(frm3,frm4) frm3=:FX:*(-(:R0:/R7)^2*(0.5*COS(2*TET7)- frm4=COS(4*TET7))-1.5*(:R0:/R7)^4*COS(4*TET7)) (STORED SYTH IS :frm3::frm4: with imat>100) (STORED SY/T IS STRY/SYTH with imat>100) char(ff1,ff2,ff3,Tf1,Rf1) real(rf2) rf2=R0**2 Rf1=(:Rf2:/(YG^2+XG^2)) Tf1=ATAN(YG/XG) ff1=:FX:*(-:Rf1:*(0.5*SIN(2*:Tf1:)+ ff2=SIN(4*:Tf1:))+ ff3=1.5*:Rf1:^2*SIN(4*:Tf1:)) (STORED VAR SXYT IS :ff1::ff2::ff3: with imat>100) (STORED VAR XY/T IS STXY/SXYT with imat>100) SAVE7END ************************************************************ Group 8. Terms & Devices USP = T ; USPDBG= F UTCPLT = T ; USPIMB= F UAUTO = T ; UGTGRD= F USPVTK = T ; USPTER= F USCANX = T ; USCANY= T USCANZ = T MXLEV = 0 ;MYLEV = 0 ;MZLEV = 0 DOMAT = -1 CELLST = 10 ; FACEST= 10 MINPRP = -1 ; MAXPRP= 250 UMXLEV = 4 ; UMXCLS= 10000 UNOLAY = 2 ; UIOLEV= 2 UWALEV = 2 ; UGRITR= 2 UMXCRS = 16 USPREL = 7.000000E-01 ; UMNCEL= 1.000000E+00 UDVREL = 1.000000E+00 ************************************************************ Group 9. Properties * Domain material index is 160 signifying: * NOTSET SETPRPS(1,160,Q1) ENUT = 0.000000E+00 DRH1DP = 5.000000E-12 DVO1DT = 1.000000E-05 * List of user-defined materials to be read by EARTH MATFLG=T;IMAT=1 * Name *Ind. Dens. Viscos. Spec.heat Conduct. Expans. Compr. *160 7800.0 0.3 473.0 43.0 1.0E-5 1.0E-7 ************************************************************ Group 10.Inter-Phase Transfer Processes ************************************************************ Group 11.Initialise Var/Porosity Fields FIINIT(XY/T) = 1.001000E-10 ;FIINIT(SXYT) = 1.001000E-10 FIINIT(SY/T) = 1.001000E-10 ;FIINIT(SYTH) = 1.001000E-10 FIINIT(SX/T) = 1.001000E-10 ;FIINIT(SXTH) = 1.001000E-10 FIINIT(TET7) = 1.001000E-10 ;FIINIT(R7 ) = 1.001000E-10 FIINIT(EPSZ) = 1.001000E-10 ;FIINIT(EPSX) = 1.001000E-10 FIINIT(EPSY) = 1.001000E-10 ;FIINIT(STXY) = 1.001000E-10 FIINIT(STRZ) = 1.001000E-10 ;FIINIT(STRY) = 1.001000E-10 FIINIT(STRX) = 1.001000E-10 ;FIINIT(PRPS) = 1.600000E+02 No PATCHes used for this Group INIADD = F ************************************************************ Echo save-block settings for Group 11 ************************************************************ Group 12. Convection and diffusion adjustments No PATCHes used for this Group ************************************************************ Group 13. Boundary & Special Sources EGWF = T ************************************************************ Echo save-block settings for Group 13 SAVE13BEGIN real(r02) r02 = R0**2 ***** TOP : V - normal ****** char(fV1,fV2,TV1,RV1) RV1=(:R02:/(:LY:^2+XG^2)) TV1=ATAN(:LY:/XG) fV1=:FX:*(-:RV1:*(0.5*COS(2*:TV1:)- fV2=COS(4*:TV1:))-1.5*:RV1:^2*COS(4*:TV1:)) (source of DISY at TOP is COVAL(FIXFLU,:fV1::fV2:)!VOLU) ***** TOP : U - tangential ****** char(fU1,fU2,TU1,RU1) RU1=(:R02:/(:LY:^2+XG^2)) TU1=ATAN(:LY:/XG) fU1=:FX:*(-:RU1:*(0.5*SIN(2*:TU1:)+ fU2=SIN(4*:TU1:))+1.5*:RU1:^2*SIN(4*:TU1:)) (source of DISX at TOP is COVAL(FIXFLU,:fU1::fU2:)!VOLU) (STORED VAR zzz7 IS :fU1::fU2:) ***** RIGHT : U - normal ****** char(fU3,fU4,TU2,RU2,fZZ1,fZZ2) RU2=(:R02:/(:LX:^2+YG^2)) TU2=ATAN(YG/:LX:) fU3=:FX:*(1-:RU2:*(1.5*COS(2*:TU2:)+ fU4=COS(4*:TU2:))+1.5*:RU2:^2*COS(4*:TU2:)) (source of DISX at RIGHT is COVAL(FIXFLU,:fU3::fU4:)!VOLU) (source of DISX at RIGHT is COVAL(FIXFLU,-4.e7*YG)!VOLU) (STORED VAR zzz7 IS :fU3::fU4:) fZZ1=:FX:*(1-:RU2:*(1.5*COS(2*:TU2:) fZZ2=+COS(4*:TU2:))) fZZ1=:RU2:*(1.5*COS(2*:TU2:) fZZ2=+COS(4*:TU2:)) (STORED VAR ZZZ7 IS :FZZ1::FZZ2:) (STORED VAR ZZZ7 IS :RU2:) ***** RIGHT : V - tangential ****** char(fV3,fV4,TV2,RV2) RV2=(:R02:/(:LX:^2+YG^2)) TV2=ATAN(YG/:LX:) fV3=:FX:*(-:RV2:*(0.5*SIN(2*:TV2:)+ fV4=SIN(4*:TV2:))+1.5*:RV2:^2*SIN(4*:TV2:)) (source of DISY at RIGHT is COVAL(FIXFLU,:fV3::fV4:)!VOLU) (source of DISX at LEFT is COVAL(1,0)!VOLU) (source of DISY at BOT is COVAL(1,0)!VOLU) SAVE13END ************************************************************ Group 14. Downstream Pressure For PARAB ************************************************************ Group 15. Terminate Sweeps LSWEEP = 800 RESFAC = 1.000000E-07 ************************************************************ Group 16. Terminate Iterations ************************************************************ Group 17. Relaxation ************************************************************ Group 18. Limits ************************************************************ Group 19. EARTH Calls To GROUND Station STRA = T PARSOL = F ISG21 = 400 ISG50 = 1 ISG52 = 3 CSG10 ='q1' SPEDAT(SET,MATERIAL,160,L,T) ************************************************************ Group 20. Preliminary Printout ************************************************************ Group 21. Print-out of Variables DISTIL=T EX(DISY)= 3.649E-04 EX(DISX)= 1.184E-03 EX(SXYT)= 1.296E+03 EX(SY/T)= 1.234E+00 EX(SYTH)= 1.445E+03 EX(SX/T)= 1.055E+00 EX(SXTH)= 9.872E+03 EX(TET7)= 7.854E-01 EX(R7 )= 1.351E+00 EX(EPSZ)= 3.253E-04 EX(EPSX)= 9.710E-04 EX(EPSY)= 2.903E-04 EX(STXY)= 1.327E+03 EX(STRZ)= 2.444E-13 EX(STRY)= 1.477E+03 EX(STRX)= 9.801E+03 EX(XY/T)= 1.206E+00 EX(ZZZ7)= 9.338E+03 ************************************************************ Group 22. Monitor Print-Out IXMON = 7 ;IYMON = 1 ;IZMON = 1 NPRMON = 100000 NPRMNT = 1 TSTSWP = -1 ************************************************************ Group 23.Field Print-Out & Plot Control NPRINT = 100000 NXPRIN = 3 NYPRIN = 4 ISWPRF = 1 ;ISWPRL = 100000 No PATCHes used for this Group ************************************************************ Group 24. Dumps For Restarts GVIEW(P,-1.445024E-01,2.191776E-01,9.649254E-01) GVIEW(UP,-3.081209E-02,9.736905E-01,-2.257833E-01) > DOM, SIZE, 2.000000E+00, 2.000000E+00, 5.000000E-01 > DOM, MONIT, 1.300000E+00, 1.000000E-01, 2.500000E-01 > DOM, SCALE, 1.000000E+00, 1.000000E+00, 1.000000E+00 > DOM, INCREMENT, 1.000000E-02, 1.000000E-02, 5.000000E-01 > GRID, RSET_X_1, 10, 0.000000E+00 > GRID, RSET_Y_1, 10, 1.000000E+00 > GRID, RSET_Z_1, 1, 1.000000E+00 > OBJ, NAME, LEFT > OBJ, POSITION, 0.000000E+00, 0.000000E+00, 0.000000E+00 > OBJ, SIZE, 0.000000E+00, 2.000000E+00, 5.000000E-01 > OBJ, GEOMETRY, cube11 > OBJ, ROTATION24, 1 > OBJ, TYPE, PLATE > OBJ, NAME, BOT > OBJ, POSITION, 0.000000E+00, 0.000000E+00, 0.000000E+00 > OBJ, SIZE, 2.000000E+00, 0.000000E+00, 5.000000E-01 > OBJ, GEOMETRY, cube11 > OBJ, ROTATION24, 1 > OBJ, TYPE, PLATE > OBJ, NAME, TOP > OBJ, POSITION, 0.000000E+00, 2.000000E+00, 0.000000E+00 > OBJ, SIZE, 2.000000E+00, 0.000000E+00, 5.000000E-01 > OBJ, GEOMETRY, cube11 > OBJ, ROTATION24, 1 > OBJ, TYPE, PLATE > OBJ, NAME, RIGHT > OBJ, POSITION, 2.000000E+00, 0.000000E+00, 0.000000E+00 > OBJ, SIZE, 0.000000E+00, 2.000000E+00, 5.000000E-01 > OBJ, GEOMETRY, cube11 > OBJ, ROTATION24, 1 > OBJ, TYPE, PLATE > OBJ, NAME, HOLE > OBJ, POSITION, 0.000000E+00, 0.000000E+00, 0.000000E+00 > OBJ, SIZE, 5.000000E-01, 5.000000E-01, 5.000000E-01 > OBJ, GEOMETRY, quarter-cylinder > OBJ, ROTATION24, 1 > OBJ, GRID, NO > OBJ, TYPE, BLOCKAGE > OBJ, MATERIAL, 198,Solid with smooth-wall friction ************************************************************ STOP