Cannot output Plastic Strain Upper/Lower
Altair Employeehi guys it's me again. I'm still learning about radioss here...now I have another confusing situation. Below is my engine file. Can someone also explain to me what the difference is between the SHELL Lower and Upper EPSP and the ELEM/EPSP? ](*,)
The weird thing is for the same file for luggage retention I can read the Upper/Lower Plastic strains but when I use it in my R14 model I can't read it. I'm using animator a4_143 for post processing.
Thanks for the help guys..
/TITLE
2KW_R14_V000_0000.rad
/VERS/100
/DT/NODA/CST
6.700000e-001 5.000000e-004
/ANIM/DT
0.000000e-000 1.000000e+001
/TFILE
1.000000e-003
/RFILE
500000 0 0
/PRINT/100
#
/RUN/2KW_R14_BELTANCHORAGE_000/1
2.600000e+002
/MON/ON
# Animation Output
/ANIM/SHELL/EPSP/UPPER
/ANIM/SHELL/EPSP/LOWER
#
/ANIM/ELEM/ENER
/ANIM/ELEM/EPSP
/ANIM/ELEM/HOURG
/ANIM/ELEM/VONM
/ANIM/ELEM/SIGX
/ANIM/ELEM/SIGY
/ANIM/ELEM/SIGZ
/ANIM/VECT/VEL
/ANIM/VECT/CONT
/ANIM/VECT/FOPT
/ANIM/NODA/DT
/ANIM/NODA/DMAS
/ANIM/MASS
/ANIM/SPRING/FORC
/ANIM/BEAM/FORC
/ANIM/ELEM/THIC
/ANIM/SHELL/TENS/STRESS/MEMB
/ANIM/SHELL/TENS/STRESS/UPPER
/ANIM/SHELL/TENS/STRESS/LOWER
/ANIM/SHELL/TENS/STRESS/BEND
/ANIM/SHELL/TENS/STRAIN/MEMB
/ANIM/SHELL/TENS/STRAIN/UPPER
/ANIM/SHELL/TENS/STRAIN/LOWER
/ANIM/SHELL/TENS/STRAIN/BEND
/END/ENGINE
#
#
/BEGIN
2KW_R14_V000_0000
100 0
kg mm s
kg mm s
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#- 1. CONTROL CARDS:
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/TITLE
2KW_R14_BELTANCHORAGE_000
/SPMD
# DOMDEC SPMD DECMOT
0 0 0
/IOFLAG
# IPRI IRTYP IGTYP IOUTP IOUTYY IROOTYY IRTYP_R
0 0 0 0 0 0 0
/ANALY
# N2D3D INTEG IPARITH ISUB
0 0 0 0
/DEF_SOLID
# I_SOLID ISMSTR ISTRAIN IFRAME
0 0 0 0
# B_HOURG B_SSTRN
12 0
/DEF_SHELL
# ISHELL ISMSTR ITHICK IPLAS ISTRAIN I_SH3N
0 0 0 0 0 1
/SHFRA/V4
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#include ./2KW_R14_BELTANCHORAGE_000_0000.rad
/END
OUT FILE
2KW_2KW_R14_V000_0001.out
************************************************************************
** **
** **
** RADIOSS ENGINE 11.0 **
** **
** Non-linear Finite Element Analysis Software **
** from Altair Engineering, Inc. **
** **
** **
** Linux 64 bits, Intel compiler, Intel MPI **
** **
** **
** **
** Build tag: 0555074_872311.0_20710 **
************************************************************************
** COPYRIGHT © 1986-2011 Altair Engineering, Inc. **
** All Rights Reserved. Copyright notice does not imply publication. **
** Contains trade secrets of Altair Engineering Inc. **
** Decompilation or disassembly of this software strictly prohibited. **
************************************************************************
NUMBER OF SPMD DOMAINS 16
NUMBER OF THREADS PER DOMAIN 1
NUMBER OF HMPP PROCESSES 16
COMPUTATION HARDWARE DESCRIPTION
CPU# HOSTNAME CPU TYPE, FREQUENCY AND MEMORY
1 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
2 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
3 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
4 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
5 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
6 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
7 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
8 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
9 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
10 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
11 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
12 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
13 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
14 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
15 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
16 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
************************************************************************
2KW_2KW_R14_V000D012KW_R14_V000_0000.rad
FINAL TIME . . . . . . . . . . . . . . . . . . . 260.0000
TIME INTERVAL FOR TIME HISTORY PLOTS . . . . . . 0.1000000E-02
TIME STEP SCALE FACTOR . . . . . . . . . . . . . 0.9000000
MINIMUM TIME STEP . . . . . . . . . . . . . . . 0.000000
NODAL TIME STEP SCALE FACTOR . . . . . . . . . . 0.6700000
NODAL MINIMUM TIME STEP. . . . . . . . . . . . . 0.5000000E-03
MIN. TIME FLAG (1:STOP 3:INCREASE MASS). . . . . 3
BRICK TIME STEP SCALE FACTOR . . . . . . . . . . 0.9000000
BRICK MINIMUM TIME STEP. . . . . . . . . . . . . 0.000000
MIN. TIME STEP FLAG (1:STOP RUN, 2:DELETE BRICK) 0
QUAD TIME STEP SCALE FACTOR. . . . . . . . . . . 0.9000000
QUAD MINIMUM TIME STEP . . . . . . . . . . . . . 0.000000
MIN. TIME STEP FLAG (1:STOP RUN, 2:DELETE QUAD). 0
SHELL TIME STEP SCALE FACTOR . . . . . . . . . . 0.9000000
SHELL MINIMUM TIME STEP. . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE, 3:SMALL STRAIN) 0
TRUSS TIME STEP SCALE FACTOR . . . . . . . . . . 0.9000000
TRUSS MINIMUM TIME STEP. . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE). . . . . . . . 0
BEAM TIME STEP SCALE FACTOR. . . . . . . . . . . 0.9000000
BEAM MINIMUM TIME STEP . . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE). . . . . . . . 0
SPRING TIME STEP SCALE FACTOR. . . . . . . . . . 0.9000000
SPRING MINIMUM TIME STEP . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE). . . . . . . . 0
AIRBAG TIME STEP SCALE FACTOR. . . . . . . . . . 0.9000000
AIRBAG MINIMUM TIME STEP . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP). . . . . . . . . . . . . 0
INTERFACE TYPE 7 TIME STEP SCALE FACTOR. . . . . 0.9000000
INTERFACE TYPE 7 MINIMUM TIME STEP . . . . . . . 0.000000
MIN. TIME FLAG(1:STOP, 2:REMOVE NODE FROM INTERF) 0
PRINTOUT CYCLE FREQUENCY . . . . . . . . . . . . 100
RESTART CYCLE FREQUENCY. . . . . . . . . . . . . *****
MAXIMUM RESTART WRITE BEFORE OVERWRITE . . . . . 0
INVERS: INPUT DECK VERSION . . . . . . . . . . . 100
ITTYP : FLAG FOR TYPE OF T-FILE. . . . . . . . . 4
TIME FOR FIRST ANIMATION-FILE PLOT . . . . . . . 0.000000
TIME INTERVAL FOR ANIMATION-FILE PLOTS . . . . . 10.00000
SENSOR FOR ANIMATION-FILE PLOTS. . . . . . . . . 0
TIME INTERVAL FOR SENSOR ANIMATION-FILE PLOTS. . 0.000000
VARIABLE SAVED ON ANIMATION FILES (1: YES) :
PLASTIC STRAIN. . . . . . 1
DENSITY (SOLID ONLY). 0
SPECIFIC ENERGY . . . . . 1
HOURGLASS ENERGY. . . . . 1
TEMPERATURE (SOLID ONLY). 0
THICKNESS (SHELL ONLY). 1
PRESSURE (SOLID ONLY). 0
VON MISES . . . . . . . . 1
TURBULENT ENERGY (FLUID). 0
TURBULENT VISCOSITY(FLUID) 0
VORTICITY (FLUID) . . . . 0
VECTOR SAVED ON ANIMATION FILES (1: YES) :
VELOCITY VECTOR . . . . . 1
DISPLACEMENT VECTOR . . . 0
ACCELERATION VECTOR . . . 0
CONTACT FORCES. . . . . . 1
INTERNAL FORCES . . . . . 0
EXTERNAL FORCES . . . . . 0
SECTION RBY RWALL FORCES. 1
ROTATIONAL VELOCITY VECTOR 0
CONTACT PRESSURE (VECTORS) 0
SHELL TENSOR SAVED ON ANIMATION FILES (1: YES) :
MEMBRANE STRESS . . . . . 0
BENDING STRESS(MOMENT/T^2) 0
UPPER LAYER STRESS. . . . 0
LOWER LAYER STRESS. . . . 0
MEMBRANE STRAIN . . . . . 0
CURVATURE . . . . . . . . 0
UPPER LAYER STRAIN. . . . 0
LOWER LAYER STRAIN. . . . 0
NODAL MASS SAVED ON ANIMATION FILES (1: YES) : 1
KEEP DELETED ELEMENT (1: YES) : 0
INITIAL TIME STEP. . . . . . . . . . . . . . . . 0.000000
MAXIMUM TIME STEP. . . . . . . . . . . . . . . . 0.1000000E+31
PARALLEL ARITHMETIC ON
MOMENTUM UPWIND : UNIFORM & ISOTROPIC . . . . .
Upwind coefficients taken from material input .
DONEA GRID VELOCITY COMPUTATION METHOD . . . . .
ALE PARAMETER ALPHA . . . . . . . . . . . . . . 0.000000
ALE PARAMETER GAMMA . . . . . . . . . . . . . . 0.000000
CWX X-MESH VELOCITY FACTOR . . . . . . . . . . . 0.000000
CWY Y-MESH VELOCITY FACTOR . . . . . . . . . . . 0.000000
CWZ Z-MESH VELOCITY FACTOR . . . . . . . . . . . 0.000000
VMIN MINIMUM VOLUME . . . . . . . . . . . . . . -0.1000000E+31
NUMBER OF INTERFACES TO BE ELIMINATED. . . . . . 0
NUMBER OF SOLID ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF QUAD ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SHELL ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF TRUSS ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF BEAM ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SPRING ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SH_3N ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SPH PARTICLES BLOCKS TO BE ELIMINATED 0
NUMBER OF RIGID LINKS . . . . . . . . . . . . . 0
NUMBER OF ALE LINKS . . . . . . . . . . . . . . 0
NUMBER OF NEW BOUNDARY CONDITIONS. . . . . . . . 0
Answers
-
hi guys it's me again. I'm still learning about radioss here...now I have another confusing situation. Below is my engine file. Can someone also explain to me what the difference is between the SHELL Lower and Upper EPSP and the ELEM/EPSP? ](*,)
The weird thing is for the same file for luggage retention I can read the Upper/Lower Plastic strains but when I use it in my R14 model I can't read it. I'm using animator a4_143 for post processing.
Thanks for the help guys..
/TITLE
2KW_R14_V000_0000.rad
/VERS/100
/DT/NODA/CST
6.700000e-001 5.000000e-004
/ANIM/DT
0.000000e-000 1.000000e+001
/TFILE
1.000000e-003
/RFILE
500000 0 0
/PRINT/100
#
/RUN/2KW_R14_BELTANCHORAGE_000/1
2.600000e+002
/MON/ON
# Animation Output
/ANIM/SHELL/EPSP/UPPER
/ANIM/SHELL/EPSP/LOWER
#
/ANIM/ELEM/ENER
/ANIM/ELEM/EPSP
/ANIM/ELEM/HOURG
/ANIM/ELEM/VONM
/ANIM/ELEM/SIGX
/ANIM/ELEM/SIGY
/ANIM/ELEM/SIGZ
/ANIM/VECT/VEL
/ANIM/VECT/CONT
/ANIM/VECT/FOPT
/ANIM/NODA/DT
/ANIM/NODA/DMAS
/ANIM/MASS
/ANIM/SPRING/FORC
/ANIM/BEAM/FORC
/ANIM/ELEM/THIC
/ANIM/SHELL/TENS/STRESS/MEMB
/ANIM/SHELL/TENS/STRESS/UPPER
/ANIM/SHELL/TENS/STRESS/LOWER
/ANIM/SHELL/TENS/STRESS/BEND
/ANIM/SHELL/TENS/STRAIN/MEMB
/ANIM/SHELL/TENS/STRAIN/UPPER
/ANIM/SHELL/TENS/STRAIN/LOWER
/ANIM/SHELL/TENS/STRAIN/BEND
/END/ENGINE
#
#
/BEGIN
2KW_R14_V000_0000
100 0
kg mm s
kg mm s
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#- 1. CONTROL CARDS:
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/TITLE
2KW_R14_BELTANCHORAGE_000
/SPMD
# DOMDEC SPMD DECMOT
0 0 0
/IOFLAG
# IPRI IRTYP IGTYP IOUTP IOUTYY IROOTYY IRTYP_R
0 0 0 0 0 0 0
/ANALY
# N2D3D INTEG IPARITH ISUB
0 0 0 0
/DEF_SOLID
# I_SOLID ISMSTR ISTRAIN IFRAME
0 0 0 0
# B_HOURG B_SSTRN
12 0
/DEF_SHELL
# ISHELL ISMSTR ITHICK IPLAS ISTRAIN I_SH3N
0 0 0 0 0 1
/SHFRA/V4
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#include ./2KW_R14_BELTANCHORAGE_000_0000.rad
/END
OUT FILE
2KW_2KW_R14_V000_0001.out
************************************************************************
** **
** **
** RADIOSS ENGINE 11.0 **
** **
** Non-linear Finite Element Analysis Software **
** from Altair Engineering, Inc. **
** **
** **
** Linux 64 bits, Intel compiler, Intel MPI **
** **
** **
** **
** Build tag: 0555074_872311.0_20710 **
************************************************************************
** COPYRIGHT © 1986-2011 Altair Engineering, Inc. **
** All Rights Reserved. Copyright notice does not imply publication. **
** Contains trade secrets of Altair Engineering Inc. **
** Decompilation or disassembly of this software strictly prohibited. **
************************************************************************
NUMBER OF SPMD DOMAINS 16
NUMBER OF THREADS PER DOMAIN 1
NUMBER OF HMPP PROCESSES 16
COMPUTATION HARDWARE DESCRIPTION
CPU# HOSTNAME CPU TYPE, FREQUENCY AND MEMORY
1 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
2 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
3 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
4 shiva014.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8161 MB swap
5 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
6 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
7 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
8 shiva013.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8162 MB swap
9 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
10 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
11 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
12 shiva012.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
13 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
14 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
15 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
16 shiva011.edag.com.my Intel® Xeon® CPU 5160 @ 3.00GHz (x86_64), 3000 MHz, 7969 MB RAM, 8189 MB swap
************************************************************************
2KW_2KW_R14_V000D012KW_R14_V000_0000.rad
FINAL TIME . . . . . . . . . . . . . . . . . . . 260.0000
TIME INTERVAL FOR TIME HISTORY PLOTS . . . . . . 0.1000000E-02
TIME STEP SCALE FACTOR . . . . . . . . . . . . . 0.9000000
MINIMUM TIME STEP . . . . . . . . . . . . . . . 0.000000
NODAL TIME STEP SCALE FACTOR . . . . . . . . . . 0.6700000
NODAL MINIMUM TIME STEP. . . . . . . . . . . . . 0.5000000E-03
MIN. TIME FLAG (1:STOP 3:INCREASE MASS). . . . . 3
BRICK TIME STEP SCALE FACTOR . . . . . . . . . . 0.9000000
BRICK MINIMUM TIME STEP. . . . . . . . . . . . . 0.000000
MIN. TIME STEP FLAG (1:STOP RUN, 2:DELETE BRICK) 0
QUAD TIME STEP SCALE FACTOR. . . . . . . . . . . 0.9000000
QUAD MINIMUM TIME STEP . . . . . . . . . . . . . 0.000000
MIN. TIME STEP FLAG (1:STOP RUN, 2:DELETE QUAD). 0
SHELL TIME STEP SCALE FACTOR . . . . . . . . . . 0.9000000
SHELL MINIMUM TIME STEP. . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE, 3:SMALL STRAIN) 0
TRUSS TIME STEP SCALE FACTOR . . . . . . . . . . 0.9000000
TRUSS MINIMUM TIME STEP. . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE). . . . . . . . 0
BEAM TIME STEP SCALE FACTOR. . . . . . . . . . . 0.9000000
BEAM MINIMUM TIME STEP . . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE). . . . . . . . 0
SPRING TIME STEP SCALE FACTOR. . . . . . . . . . 0.9000000
SPRING MINIMUM TIME STEP . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP, 2:DELETE). . . . . . . . 0
AIRBAG TIME STEP SCALE FACTOR. . . . . . . . . . 0.9000000
AIRBAG MINIMUM TIME STEP . . . . . . . . . . . . 0.000000
MIN. TIME FLAG (1:STOP). . . . . . . . . . . . . 0
INTERFACE TYPE 7 TIME STEP SCALE FACTOR. . . . . 0.9000000
INTERFACE TYPE 7 MINIMUM TIME STEP . . . . . . . 0.000000
MIN. TIME FLAG(1:STOP, 2:REMOVE NODE FROM INTERF) 0
PRINTOUT CYCLE FREQUENCY . . . . . . . . . . . . 100
RESTART CYCLE FREQUENCY. . . . . . . . . . . . . *****
MAXIMUM RESTART WRITE BEFORE OVERWRITE . . . . . 0
INVERS: INPUT DECK VERSION . . . . . . . . . . . 100
ITTYP : FLAG FOR TYPE OF T-FILE. . . . . . . . . 4
TIME FOR FIRST ANIMATION-FILE PLOT . . . . . . . 0.000000
TIME INTERVAL FOR ANIMATION-FILE PLOTS . . . . . 10.00000
SENSOR FOR ANIMATION-FILE PLOTS. . . . . . . . . 0
TIME INTERVAL FOR SENSOR ANIMATION-FILE PLOTS. . 0.000000
VARIABLE SAVED ON ANIMATION FILES (1: YES) :
PLASTIC STRAIN. . . . . . 1
DENSITY (SOLID ONLY). 0
SPECIFIC ENERGY . . . . . 1
HOURGLASS ENERGY. . . . . 1
TEMPERATURE (SOLID ONLY). 0
THICKNESS (SHELL ONLY). 1
PRESSURE (SOLID ONLY). 0
VON MISES . . . . . . . . 1
TURBULENT ENERGY (FLUID). 0
TURBULENT VISCOSITY(FLUID) 0
VORTICITY (FLUID) . . . . 0
VECTOR SAVED ON ANIMATION FILES (1: YES) :
VELOCITY VECTOR . . . . . 1
DISPLACEMENT VECTOR . . . 0
ACCELERATION VECTOR . . . 0
CONTACT FORCES. . . . . . 1
INTERNAL FORCES . . . . . 0
EXTERNAL FORCES . . . . . 0
SECTION RBY RWALL FORCES. 1
ROTATIONAL VELOCITY VECTOR 0
CONTACT PRESSURE (VECTORS) 0
SHELL TENSOR SAVED ON ANIMATION FILES (1: YES) :
MEMBRANE STRESS . . . . . 0
BENDING STRESS(MOMENT/T^2) 0
UPPER LAYER STRESS. . . . 0
LOWER LAYER STRESS. . . . 0
MEMBRANE STRAIN . . . . . 0
CURVATURE . . . . . . . . 0
UPPER LAYER STRAIN. . . . 0
LOWER LAYER STRAIN. . . . 0
NODAL MASS SAVED ON ANIMATION FILES (1: YES) : 1
KEEP DELETED ELEMENT (1: YES) : 0
INITIAL TIME STEP. . . . . . . . . . . . . . . . 0.000000
MAXIMUM TIME STEP. . . . . . . . . . . . . . . . 0.1000000E+31
PARALLEL ARITHMETIC ON
MOMENTUM UPWIND : UNIFORM & ISOTROPIC . . . . .
Upwind coefficients taken from material input .
DONEA GRID VELOCITY COMPUTATION METHOD . . . . .
ALE PARAMETER ALPHA . . . . . . . . . . . . . . 0.000000
ALE PARAMETER GAMMA . . . . . . . . . . . . . . 0.000000
CWX X-MESH VELOCITY FACTOR . . . . . . . . . . . 0.000000
CWY Y-MESH VELOCITY FACTOR . . . . . . . . . . . 0.000000
CWZ Z-MESH VELOCITY FACTOR . . . . . . . . . . . 0.000000
VMIN MINIMUM VOLUME . . . . . . . . . . . . . . -0.1000000E+31
NUMBER OF INTERFACES TO BE ELIMINATED. . . . . . 0
NUMBER OF SOLID ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF QUAD ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SHELL ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF TRUSS ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF BEAM ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SPRING ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SH_3N ELEMENT BLOCKS TO BE ELIMINATED 0
NUMBER OF SPH PARTICLES BLOCKS TO BE ELIMINATED 0
NUMBER OF RIGID LINKS . . . . . . . . . . . . . 0
NUMBER OF ALE LINKS . . . . . . . . . . . . . . 0
NUMBER OF NEW BOUNDARY CONDITIONS. . . . . . . . 0
Check your default '/DEF_SHELL' card. You could read the details from the help about 'DEF_SHELL'.
You should use 'Istrain=1' in your default shell card.
Another way is changing 'Istrain=1' from '/Prop/Shell'. If you have not defined anything in the /Prop/shell card it uses /Def_Shell card.
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thanks! i will give this a try..the strange thing is in my previous model the ISTRAIN=0 always gave me the plastics strains lower and upper..oh well i have to check my 18 include files if I have control cards left somewhere there...will give updates if I have someting [-o<
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i changed ISTRAIN=1 and still unable to extract Upper/Lower Plastic strains....any more tips? thinks
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i just noticed something new. the previous runs that i had that has no issues at all was running on a different version of radios xxxx_12310 and the one that has issues where running on xxxx_20710..could this be a bug on the current version released on Nov.11? I emailed altair support but no reply since Wednesday .
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i just noticed something new. the previous runs that i had that has no issues at all was running on a different version of radios xxxx_12310 and the one that has issues where running on xxxx_20710..could this be a bug on the current version released on Nov.11? I emailed altair support but no reply since Wednesday .
have you tried radioss 11_201 ??
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it's fixed already...it's strange nothing was wrong from the start...i moved the results to a different folder now they are giving me the results i needed....no fixing needed..
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