VM-R029-T7 190 Input Listing


/COM,ANSYS MEDIA REL. 2024R2 (05/10/2024) REF. VERIF. MANUAL: REL. 2024R2
/VERIFY,VMR029-T7-190
/TITLE,VMR029-T7-190,LARGE DISPLACEMENT ELASTRIC RESPONSE OF A HINGED SPHERICAL SHELL UNDER UNIFORM PRESSURE LOADING
/COM, REF. NAFEMS ASSEMBLY BENCHMARK TESTS FOR 3D BEAMS AND SHELLS
/COM, TEST 3DNLG-7

/PREP7
L=1570
T=100
P=0.1
ET,1,190
MP,EX,1,69
MP,NUXY,1,0.3
K,1,
K,6,5*L/8,,0.00020285*((5*L/8)*(3*L/8))
K,9,L,,0
LARC,       1,       9,       6
K,15,,3*L/4,0.00020285*((3*L/4)*(L/4))
K,17,,L,0
LARC,       1,      17,      15
ADRAG,1,,,,,,2
VEXT,ALL,,,0,0,T/2,,,,
VEXT,1,,,0,0,-T/2,,,,
K,111,10000,1570,10000
K,112,10000,1570,-10000
K,113,-10000,1570,-10000
K,114,-10000,1570,10000
A,111,112,113,114
VSBA,1,12,,,KEEP
VSBA,2,12
VDELE,1,3
LESIZE,ALL,,,8
LESIZE,10,,,1
LESIZE,11,,,1
LESIZE,12,,,1
LESIZE,13,,,1
LESIZE,18,,,1
LESIZE,19,,,1
LESIZE,20,,,1
LESIZE,21,,,1
VMESH,ALL
NUMMRG,ALL, , , ,LOW
DL,26,,ALL,
DL,5,,ALL,
DL,2,,ALL,
DL,1,,ALL,
VSEL,S,,,4
ESLV,S
SFE,ALL,6,PRES,,P
ALLSEL,ALL
ESEL,S,,,1
ESEL,A,,,35
ESEL,A,,,92
CM,ELESOL,ELEM
ALLSEL,ALL
FINISH

/SOLU
NLGEOM,ON
NSUBST,200,1000,25
OUTRES,ALL,ALL
ARCLEN,ON,,
AUTOTS,-1
/OUT,SCRATCH
SOLVE
FINISH
/SHOW,,jpeg

/OUT
/POST26
*DIM,X,TABLE,11,1
*DIM,Y,TABLE,11,1
X(1,1)= 0
Y(1,1)= 0
X(2,1)= 30
Y(2,1)= 0.042
X(3,1)= 60
Y(3,1)= 0.06
X(4,1)= 90
Y(4,1)= 0.063
X(5,1)= 120
Y(5,1)= 0.056
X(6,1)= 150
Y(6,1)= 0.048
X(7,1)= 180
Y(7,1)= 0.037
X(8,1)= 210
Y(8,1)= 0.031
X(9,1)= 240
Y(9,1)= 0.03
X(10,1)= 270
Y(10,1)= 0.05
X(11,1)= 300
Y(11,1)= 0.096
/XRANGE,0,420
/YRANGE,0,0.1
/AXLAB,X,CENTRAL DEFLECTION
/AXLAB,Y,APPLIED PRESSURE
/COLOR,CURVE,YGRE
*VPLOT,X(1,1),Y(1,1)
/NOERASE
NSOL,2,138,U,Z,DISP.
PROD,3,2,,,DISP.,,,-1.0,0,0,
PROD,7,1,,,LOAD,,,0.1,0,0,
/COLOR,CURVE,MRED
XVAR,3
PLVAR,7
PRVAR,1,,3,7
FINISH

/POST1
SET, , ,1, ,1.012, ,
*GET,VAL8,NODE,138,U,Z
*SET,UA_8,-1*VAL8
*GET,VAL9,NODE,219,U,Z
*SET,UA_9,-1*VAL9
*GET,VAL7,NODE,57,U,Z
*SET,UA_7,-1*VAL7
*DIM,LABEL1,CHAR,1,2
LABEL1(1,1) = '0.1012'
LABEL1(1,2) = '      '
*DIM,VALUE1,CHAR,1,2
VALUE1(1,1) = '303.1'
VALUE1(1,2) = '     '
*DIM,LABEL2,CHAR,1,3
LABEL2(1,1) = ' TOP '
LABEL2(1,2) = ' MID.'
LABEL2(1,3) = 'BOTT.'
*DIM,ERROR1,,1,3
*VFILL,ERROR1(1,1),DATA,UA_8
*VFILL,ERROR1(1,2),DATA,UA_7
*VFILL,ERROR1(1,3),DATA,UA_9

/OUT,
/COM,
/COM,  -------------      CENTRAL DISPLACEMENT      -------------
/COM,
/COM,                  |   NAFEMS   |       Mechanical APDL         |
/COM,         |  LOAD  |  NUM.RES.  |  LAYER  	|  	SOL.190  |
/COM,
*VWRITE,LABEL1(1,1),VALUE1(1,1),LABEL2(1,1),ERROR1(1,1)
(1X,'           ',A6,'     ',A5,'       ',A5,'    ',F12.3)
*VWRITE,LABEL1(1,2),VALUE1(1,2),LABEL2(1,2),ERROR1(1,2)
(1X,'           ',A6,'     ',A5,'       ',A5,'    ',F12.3)
*VWRITE,LABEL1(1,2),VALUE1(1,2),LABEL2(1,3),ERROR1(1,3)
(1X,'           ',A6,'     ',A5,'       ',A5,'    ',F12.3)
/COM,
/COM,  ----------------------------------------------------------

ESEL,,,,ELESOL
NSLE
ESEL,ALL
PRNSOL,S,COMP
PRNSOL,EPTO,COMP

SET,1,16
*GET,PRES1,TIME
SET,1,25
*GET,PRES2,TIME
V1=PRES1*0.1
V2=PRES2*0.1
R1=V1/0.06495
R2=V2/0.03084
*DIM,VALUE,,2,2
*DIM,LABEL3,CHAR,3
*DIM,LABEL,CHAR,3
*DIM,LABEL4,CHAR,3
*VFILL,VALUE(1,1),DATA,V1,V2
*VFILL,VALUE(1,2),DATA,R1,R2
LABEL3(1) = 'LIMIT1','LIMIT2'
LABEL(1) = 'vmr029-','vmr029-'
LABEL4(1) = 't7-190','t7-190'
/OUT,vmr029-t7-190,vrt
/COM
/COM,-------------- VMR029-T7  RESULTS COMPARISON ---------------
/COM,
/COM,          |    Mechanical APDL    |   RATIO   |      INPUT      |
/COM,
/COM,SOLSH190
*VWRITE,LABEL3(1),VALUE(1,1),VALUE(1,2),LABEL(1),LABEL4(1)
(1X,A6,'        ',F12.5,'      ',F13.5,'      ',A7,A8)
/COM,
/COM,----------------------------------------------------------------
/OUT
FINISH
*LIST,vmr029-t7-190,vrt