还是有问题，如果不设置温度，就说 重力过程必须设置温度，我采用picking的方式以后还是说Gravity will be isothermal 运算出现下面这些，老大帮帮忙。
START TO READ IOSL INPUT FILE : E:\pam\练习\保险杠热冲\baoxiangang.pre
STARTING OF THE ANALYSIS : Gravity
SAVING THE SET-UP FILE : E:\pam\练习\保险杠热冲\baoxiangang_01_Gravity.pre
P O S I T I O N I N G A C T I O N
TRANSLATION ACTION .....: Initial Positioning of Blankholder
POSITION OBJECT(S)......: Blank holder
ALONG DIRECTION.........: 0,0,1
WITH MAGNITUDE..........: 0
VALUE OF THE DISPLACEMENT = 0.000000e+000
P O S I T I O N I N G A C T I O N
AUTOPOSITIONING ACTION .....: Blank Autopositioning
POSITION OBJECT(S)......: Blank
ONTO OBJECT(S)..........: Blank holder , Punch
ALONG DIRECTION.........: 0,0,1
WITH TOLERANCE..........: 0.001
VALUE OF THE DISPLACEMENT = 7.364951e+002
I O S L I N F O R M A T I O N
NUMBER OF OBJECTS : 3
OBJECT ID 3 WITH NAME Punch
OBJECT ID 4 WITH NAME Blank holder
OBJECT ID 11 WITH NAME Blank
--- AUXILLARY DEFINITION ---
NUMBER OF CURVES : 11
CURVE ID 5 WITH NAME HC
CURVE ID 6 WITH NAME curve_20
CURVE ID 7 WITH NAME curve_400
CURVE ID 8 WITH NAME curve_200
CURVE ID 9 WITH NAME curve_600
CURVE ID 10 WITH NAME curve_860
CURVE ID 16 WITH NAME BHforce_coef_-1
CURVE ID 17 WITH NAME velocity ramp curve
CURVE ID 18 WITH NAME H(d)
CURVE ID 12 WITH NAME cp_curve
CURVE ID 15 WITH NAME Constant value 0.00981 - Generated by IOSL
NUMBER OF FRAMES : 1
FRAME ID 19 WITH NAME press direction
--- ATTRIBUTE DEFINITION ---
NUMBER OF PARTS : 3
PART/MAT ID 3 ON OBJECT Punch
PART/MAT ID 4 ON OBJECT Blank holder
PART/MAT ID 11 ON OBJECT Blank
NUMBER OF CONTACTS : 2
CNTAC ID 13 ON OBJECT Punch
CNTAC ID 14 ON OBJECT Blank holder
NUMBER OF BOUNDARY COND. : 2
BOUNC ON OBJECT Punch
BOUNC ON OBJECT Blank holder
NUMBER OF ACCELERATIONS : 1
ACFLD ON OBJECT Blank
T I T L E
baoxiangang (01 : Gravity)
C O N T R O L I N F O R M A T I O N
NUMBER OF PARTS................................ 3
NUMBER OF MATERIALS............................ 2
NUMBER OF NODAL POINTS......................... 3757
NUMBER OF 8-NODE SOLID ELEMENTS................ 0
NUMBER OF SHELL/MEMBRANE ELEMENTS.............. 3886
NUMBER OF TOTAL 1-D ELEMENTS .................. 0
NUMBER OF 0-D ELEMENTS (PARTICLES) ............ 0
NUMBER OF MULTIBODY SYSTEMS.................... 0
NUMBER OF DISP. B.C. DEFINITIONS............... 2
NUMBER OF NODAL TIME HISTORY DEFINITIONS ...... 0
NUMBER OF ELEMENT TIME HISTORY DEFINITIONS .... 0
NUMBER OF B.C. ON POINTS DEFINITION............ 0
NUMBER OF LOCAL COORDINATE FRAMES.............. 1
NUMBER OF AIRBAGS ............................. 0
NUMBER OF PLIES IN COMPOSITE PLIES DATABASE.... 0
NUMBER OF RIGID BODY DEFINITIONS............... 0
NUMBER OF SECTIONS FOR TRANSMISSION FORCES..... 0
NUMBER OF LOAD CURVES.......................... 11
NUMBER OF LOOK UP TABLES....................... 0
NUMBER OF CONCENTRATED LOAD CARDS.............. 0
NUMBER OF FACE PRESSURE CARDS..(SOLIDS/SHELLS). 0
NUMBER OF BEAM PRESSURE CARDS..(BEAMS)......... 0
NUMBER OF VELOCITY CARDS....................... 0
NUMBER OF USER-DEFINED GAS CARDS .............. 0
NUMBER OF NODES WITH ADDITIONAL MASSES......... 0
NUMBER OF RIGID WALL DEFINITIONS............... 0
NUMBER OF CONSTRAINT CARDS..................... 0
NUMBER OF INITIAL VELOCITIY CARDS.............. 0
EQ.0, VELOCITIES ARE INITIALIZED TO ZERO
GT.0, INITIAL VELOCITIES ARE READ IN
NUMBER OF SLIDING SURFACES..................... 2
NUMBER OF RUPTURE MODELS....................... 0
NUMBER OF FRICTION MODELS...................... 0
NUMBER OF PRESCRIBED ACCELERATION FIELDS....... 1
NUMBER OF FLUID FORMING CELL DEFINITIONS....... 0
NUMBER OF PLINK - SPOTWELD DEFINITIONS......... 0
NUMBER OF TIED CONNECTION INTERFACES........... 0
NUMBER OF SLINK - SURFACE LINK DEFINITIONS..... 0
NUMBER OF ELINK - EDGE LINK DEFINITIONS........ 0
NUMBER OF LLINK - LINE LINK DEFINITIONS........ 0
NUMBER OF SENPT - SENSOR POINT DEFINITIONS..... 0
NUMBER OF NSMAS - NONSTRUCTURAL MASS........... 0
NUMBER OF MSTRM - MASS TRIM DEFINITION......... 0
NUMBER OF DELEM - ELEMENT ELIMINATION CARDS ... 0
NUMBER OF SENSORS.............................. 0
NUMBER OF BELT SLIPRINGS....................... 0
NUMBER OF RETRACTORS........................... 0
NUMBER OF MUSCLES.............................. 0
NUMBER OF FAST BELT SYSTEMS.................... 0
NUMBER OF GAUGES (ACCEL. IN LOCAL FRAME)....... 0
NUMBER OF NODAL DAMPING GROUPS................. 0
NUMBER OF 3-D DRIVEN ACCELERATION CARDS ....... 0
NUMBER OF 3-D DRIVEN VELOCITY CARDS ........... 0
NUMBER OF 3-D DRIVEN DISPLACEMENT CARDS ....... 0
NUMBER OF 3-D DRIVEN ANGULAR ACCEL. CARDS ..... 0
NUMBER OF 3-D DRIVEN ANGULAR VELOCITY CARDS ... 0
NUMBER OF 3-D DRIVEN ANGULAR DISPL. CARDS ..... 0
NUMBER OF 3-D DRIVEN MIN DISPLACEMENT CARDS ... 0
NUMBER OF 3-D DRIVEN MAX DISPLACEMENT CARDS ... 0
NUMBER OF SUBSTRUCTURE DEFINITIONS ............ 0
NUMBER OF TRANSFORMATION DEFINITIONS .......... 0
NUMBER OF FREEZE DEFINITION.................... 0
NUMBER OF DETONATION POINTS.................... 0
NUMBER OF ELEMENT MOMENTUM DEPOSITIONS(SOLIDS). 0
NUMBER OF NODAL MOMENTUM DEPOSITIONS........... 0
NUMBER OF ELEMENT MASS DEPOSITIONS(SOLIDS)..... 0
NUMBER OF ELEMENT ENERGY DEPOSITIONS(SOLIDS)... 0
NUMBER OF TARVER CARDS(SOLIDS)................. 0
NUMBER OF CFD PRESSURE SURFACE DEFINITIONS..... 0
TERMINATION TIME .............................. 0.10E+10
TIME HISTORY PLOT INTERVAL VALUE .............. 0.10E+01
MESH PLOT INTERVAL VALUE ...................... 0.10E+10
RESTART DUMP AT................................ 0.00E+00
NUMBER OF CYCLES BETWEEN RESTART DUMPS......... 0
NUMBER OF RUNNING RESTART FILES................ 1
CYCLE LOG FREQUENCY............................ 10
INITIAL TIME STEP SIZE......................... 0.00E+00
EQ.0.0, INITIAL TIME STEP COMPUTED INTERNALLY
USER PREFERED TIME STEP ....................... 0.00E+00
EQ.0.0, TIME STEP COMPUTED BY PROGRAM
FLAG FOR STRAIN RATE ACTIVATION ............... 1
EQ. 0, ALL STRAIN RATES SWITCHED ON (DEFAULT)
EQ. 1, ALL STRAIN RATES SWITCHED OFF
STRAIN RATE FILTER INTERVAL IN CYCLES.......... 0
EQ. 0 TOTAL STRAIN RATE WITHOUT FILTER APPLIED
EQ. 1 PLASTIC STRAIN RATE WITHOUT FILTER
GT. 1 PLASTIC STRAIN RATE WITH DEFINED FILTER CYCLES
STRAIN RATE CURVE INTERPOLATION FLAG .......... 0
EQ. 0 LINEAR
EQ. 1 LOGARITHMIC
TIME STEP SCALE FACTOR................. 0.100E+01
VELOCITY SCALING FACTOR (STRAIN RATE).. 0.100E+01
METAL-FORMING SPRING BACK FLAG ........ 1
TOTAL STRAIN CALCULATION IS BASED ON LAGRANGIAN METHOD
(DEFAULT IS INCREMENTAL)
NODAL MASS OPTION ..................... 1
EQ. 0 : STANDARD
EQ. 1 : SIMPLIFIED MASS
STRAIN ORDER FORMULATION .............. 1
THICKNESS INTEGRATION SCHEME .......... 1
EQ. 0 : UNIFORM
EQ. 1 : GAUSS
SHELL TIME STEP OPTION:
IN PLANE ............................. 0
EQ. 0 : LARGE
EQ. 1 : SMALL
BENDING ............................. -1
EQ. 0 : BEND
EQ. 1 : NOBEND
EQ.-1 : BEND LARGE
R U N E N D C R I T E R I A
PROGRESSION IS TIME
I M P L I C I T P A R A M E T E R S
NUMBER OF INCREMENTS.........................1000000000
MAXIMUM NUMBER OF NEWTON ITERATIONS.......... 20
DISPLACEMENT CONVERGENCE TOLERANCE........... -0.100E+00
ENERGY CONVERGENCE TOLERANCE................. -0.100E+02
MAXIMUM NB. OF PCG ITERATIONS SCALING FACTOR. 0.167E+00
PCG CONVERGENCE TOLERANCE.................... -0.100E-03
GRAVITY DAMPING SCALE FACTOR ................ 0.100E+01
SOLVER TYPE.................................. 1
-2 : MUMPS DIRECT OUT-OF-CORE SOLVER
-1 : MUMPS DIRECT SOLVER
0 : PCG SOLVER
DEFAULT SOLVERS
1 : DEFAULT DIRECT SYMMETRIC DOUBLE PRECISION
3 : DEFAULT ITERATIVE SYMMETRIC DOUBLE PRECISION
T E M P E R A T U R E C O N T R O L P A R A M E T E R S
FOURIER NUMBER ................................ 0.9000E+00
NUMBER OF INITIAL NODAL TEMPERATURE CARDS ..... 1
NUMBER OF IMPOSED BC NODAL TEMPERATURE CARDS .. 0
NUMBER OF IMPOSED BC NODAL FLUX CARDS ......... 0
NUMBER OF THERMAL PROPERTY SET CARDS .......... 1
O P T I O N A L S E C T I O N
SOLVER STAMP
SIGNAL YES
DATA CHECK NO
SHELL CHECK NO
SOLID CHECK NO
SOLID4N NO
AIRBAG CHECK NO
METRIC CHECK NO
MAX. RESTART DUMP 1
PIPE NO
DEBUG NO
RUN CHECK NO
RWALL KINEMATIC CHECK YES
UNIT SYSTEM
LENGTH MM
MASS KG
TIME MS
TEMPERATURE KELV
O U T P U T P A R A M E T E R S
OUTPUT FILE E:\pam\练习\保险杠热冲\baoxiangang_01_Gravity
PRINT NO
GLOBAL HISTORY OUTPUT
TOTAL CONTACT ENERGY
CONTACT FORCE
NODAL PLOT OUTPUT
CONTACT PRESSURE
SPH PLOT OUTPUT
SOLID PLOT OUTPUT
STRESS
SHELL PLOT OUTPUT
THICKNESS
STRAIN TENSOR
STRESS TENSOR
MEMB. EQUIV. STRESS
MEMB. PLASTIC STRAIN
SHELL HISTORY OUTPUT
THICKNESS
STRAIN TENSOR
STRESS TENSOR
MEMB. EQUIV. STRESS
MEMB. PLASTIC STRAIN
BEAM PLOT OUTPUT
PREFILTER NO
N O D A L P O I N T C O O R D I N A T E S
NP X-ORD Y-ORD Z-ORD
==== DATA SUPPRESSED BY NOPRINT OPTION ====
P L A T E / M E M B R A N E E L E M E N T S
ELEMENT NODE1 NODE2 NODE3 NODE4 NINT THICK/ANGLE ANGLE
==== DATA SUPPRESSED BY NOPRINT OPTION ====
NUMBER OF QUAD OR TRIANGULAR ELEMENTS = 3886
NUMBER OF MEMBRANE ELEMENTS = 0
NUMBER OF THICK SHELL ELEMENTS = 0
NB. OF SHELLS: THK INT. PTS OF PART CARD OVERWRITTEN = 3886
NB. OF SHELLS: THICKNESS OF PART CARD OVERWRITTEN = 0
T A B U L A T E D F U N C T I O N S
NUMBER OF TABULATED FUNCTIONS = 11
==== DATA SUPPRESSED BY NOPRINT OPTION ====
*** ERROR *** LOAD CURVE 5 LESS THAN 2 PTS.
blank
THERMAL PROPERTY SET NUMBER .......= 1
THERMAL MODEL .....................= 0
SPECIFIC HEAT (CONSTANT) ......... = 0.0000E+00
SPECIFIC HEAT (LOAD CURVE) ....... = 12
THERMAL CONDUCTIVITY (CONSTANT)... = 0.3600E+02
REFERENCE ENTHALPY.................= 0.0000E+00
ENTHALPY (LOAD CURVE)............. = 0
CONVERSION FACTOR................. = 0.1000E-08
(DEFAULT=0.9)
L O C A L C O O R D I N A T E F R A M E S
LOCAL FRAME NUMBER 19
FRAME ORIENTATION TYPE 1
= 0 : FRAME ATTACHED TO ENTITY
= 1 : FIXED FRAME
= 2 : SELF-ROTATED
FRAME AXIS DEF. TYPE 0
= 0 : U BASED, VIA 2 VECTORS
= 1 : U BASED, VIA 3 NODES
= 2 : T BASED, VIA 2 VECTORS
= 3 : T BASED, VIA 3 NODES
X-COMPONENT OF VECTOR 1 -0.100000E+01
Y-COMPONENT OF VECTOR 1 0.000000E+00
Z-COMPONENT OF VECTOR 1 0.000000E+00
X-COMPONENT OF VECTOR 2 0.000000E+00
Y-COMPONENT OF VECTOR 2 0.100000E+01
Z-COMPONENT OF VECTOR 2 0.000000E+00
X-COMPONENT OF VECTOR 3 0.000000E+00
Y-COMPONENT OF VECTOR 3 0.000000E+00
Z-COMPONENT OF VECTOR 3 -0.100000E+01
M A T E R I A L D E F I N I T I O N
SOLID MATERIAL MODELS
EQ.1 ELASTIC-PLASTIC
EQ.2 SOIL AND CRUSHABLE FOAM MODEL
EQ.5 VISCOELASTIC
EQ.6 JWL HIGH EXPLOSIVE
EQ.7 HYDRODYNAMIC-ELASTIC-PLASTIC
EQ.8 STEINBERG - GUINAN MODEL
EQ.9 TARVER REACTIVE BURN
EQ.11 BLATZ-KO RUBBER MODEL
EQ.12 JOHNSON-COOK MODEL
EQ.14 DATA BASE EOS
EQ.15 CRACKABLE BRITTLE-REINFORCED CONCRETE MODEL
EQ.16 ELASTIC-PLASTIC WITH DAMAGE AND FAILURE
EQ.17 MOONEY-RIVLIN RUBBER (with Hysterisis Option)
EQ.18 HART-SMITH HYPERELASTIC RUBBER
EQ.19 PRONY SERIES MOONEY-RIVLIN RUBBER
EQ.20 POLYURETHANE FOAM
EQ.21 HIGHLY COMPRESSIBLE URETHANE FOAM
EQ.22 VISCOUS FOAM
EQ.24 INELASTIC CRUSHABLE FOAM WITH HYSTERESIS
EQ.25 SPECIFIC FOAM FOR SIDE IMPACT BARRIER
EQ.26 ELASTIC-PLASTIC WITH GURSON DAMAGE
EQ.28 MURNAGHAN EOS
EQ.30 ORTHOTROPIC BI-PHASE
EQ.31 NON LINEAR FIBER BI-PHASE
EQ.35 IMPROVED FLECK FOAM MODEL
EQ.36 ELASTIC-PLASTIC WITH ELASTIC STIFFENING
EQ.37 VISCOELASTIC OGDEN MODEL, G VISCOUS MODEL
EQ.40 NO LONGER SUPPORTED
EQ.41 ADVANCED HONEYCOMB SIDE IMPACT BARRIER
EQ.42 ORTHOTROPIC/ISOTROPIC MATERIAL
EQ.45 GENERAL FOAM MODEL
EQ.46 KARMANN FOAM MODEL (based on Seeliger-Dubois model)
EQ.47 COMFORT FOAM MODEL
EQ.51 ELASTIC WITH TLF AND THERMAL DILATATION
EQ.52 ELASTIC-PLASTIC SOLID WITH FAILURE CRITERION OF KOLMOGOROV-DELL
EQ.61 ELASTIC FOR BRICK SHELL
EQ.62 ELASTIC-PLASTIC FOR BRICK SHELL
EQ.71 EWK RUPTURE MODEL - SOLID ELEMENT VERSION
EQ.99 NULL MATERIAL
EQ.80 USER-DEFINED MATERIAL (ESI EXAMPLE)
EQ.81 USER-DEFINED ELASTIC-PLASTIC MATERIAL
EQ.82 USER-DEFINED MATERIAL (ESI EXAMPLE)
EQ.83 ELASTIC-PLASTIC MATERIAL WITH JC FAILURE
SHELL MATERIAL MODELS
EQ.100 NULL MATERIAL
EQ.101 ELASTIC
EQ.102 ELASTIC-PLASTIC
EQ.103 ELASTIC-PLASTIC ITERATIVE
EQ.105 ELASTIC-PLASTIC ISOTROPIC DAMAGE
EQ.106 ELASTIC-PLASTIC ANISOTROPIC DAMAGE
EQ.117 ANISOTROPIC ELASTIC-PLASTIC(STAMPING ORIENTED)
EQ.108 ANISOTROPIC ELASTIC-PLASTIC ITERATIVE
EQ.109 ALUMINIUM ANISOTROPIC ELASTIC-PLASTIC
EQ.110 SUPERELASTIC MATERIAL
EQ.115 ELASTIC-PLASTIC WITH GURSON DAMAGE
EQ.116 TENSION-COMPRESSION ELASTIC-PLASTIC WITH DAMAGE
EQ.118 ANISOTROPIC ELASTIC-PLASTIC WITH GURSON DAMAGE
EQ.120 SUPERPLASTIC MATERIAL
EQ.121 PLASTIC FORMING VISCO-ELASTIC MATERIAL
EQ.122 OGDEN HYPERELASTIC MATERIAL
EQ.128 ANISOTROPIC ELASTIC-PLASTIC MATERIAL WITH COMBINED INSTABILITY/DUCTILE/SHEAR FAILURE
EQ.130 ORTHOTROPIC MULTILAYERED
EQ.131 SANDWICH COMPOSITE
EQ.132 FABRIC COMPOSITE
EQ.140 THERMO-VISCO-ELASTIC MATRIX, ELASTIC FIBERS
EQ.143 ELASTIC-PLASTIC WITH ELASTIC STIFFENING
EQ.150 ELASTIC MEMBRANE
EQ.151 NONLINEAR MEMBRANE
EQ.152 ELASTIC KNITTED MEMBRANE
EQ.161 ELASTIC FOR THICK SHELL
EQ.162 ELASTIC-PLASTIC FOR THICK SHELL
EQ.171 EWK RUPTURE MODEL - SHELL ELEMENT VERSION
EQ.180 USER-DEFINED MATERIAL (ESI EXAMPLE)
EQ.181 USER-DEFINED ELASTIC-PLASTIC MATERIAL
EQ.182 ORTHOTROPIC ELASTIC-PLASTIC MATERIAL (ESI)
EQ.183 ELASTIC-PLASTIC MATERIAL WITH JC FAILURE
EQ.184 USER-DEFINED MATERIAL (ESI EXAMPLE)
BAR/BEAM MATERIAL MODELS
EQ.200 NULL MATERIAL
EQ.201 ELASTIC (BEAM/BAR)
EQ.202 ELASTIC-PLASTIC (BAR)
EQ.203 IMPOSED FORCE-DISPLACEMENT (BAR)
EQ.204 NONLINEAR SPRING-DASHPOT (BAR)
EQ.205 SEAT BELT WEBBING MATERIAL (BAR)
EQ.212 IMPROVED ELASTIC-PLASTIC (BEAM)
EQ.213 ARBITRARY SECTION (BEAM)
EQ.214 STEERING COLUMN BEAM
EQ.220 6-DOF SPRING
EQ.221 SPHERICAL (CARDAN) JOINT
EQ.222 FLEXION-TORSION JOINT
EQ.223 6-DOF SPRING-BEAM
LINK MATERIAL MODELS
EQ.301 SLINK/ELINK, TIED SURFACE MATERIAL
EQ.302 PLINK MATERIAL
EQ.303 TIED SURFACE MATERIAL WITH DELAMINATION
EQ.304 ORTHOTROPIC PLASTIC TIED CONNECTION
*** ERROR *** OCCURRED IN INPUT PHASE, SEE ABOVE |
