Error in output results.

RAMGANESH · May 2016

Dear All,

I am working on the seat strength analysis ,my analysis is completed but the structure is deforming more than the expected one.Kindly give your suggestions

Thanks

Ram

<?xml version="1.0" encoding="UTF-8"?>

Rahul Rajan_21763 · May 2016

could you share us input deck?

RAMGANESH · May 2016

Dear Rahul,

Kindly find the data below.

CONTROL PARAMETERS
-------------------

IPRI : PRINTOUT FLAG . . . . . . . . . . . . . . . . 0
INVERS: MANUAL VERSION OF THIS INPUT DECK . . . . . . 110
NSUBS: NUMBER OF SUBSETS. . . . . . . . . . . . . . 1
NPART: NUMBER OF PARTS. . . . . . . . . . . . . . . 8
NUMMAT: NUMBER OF MATERIALS . . . . . . . . . . . . . 2
NUMGEO: NUMBER OF PROPERTY SETS . . . . . . . . . . . 5
NUMNOD: NUMBER OF NODAL POINTS. . . . . . . . . . . . 30635
NUMSKW: NUMBER OF SKEW REFERENCE FRAMES . . . . . . . 0
NUMBCS: NUMBER OF BOUNDARY CONDITIONS . . . . . . . . 2
NUMFRAM: NUMBER OF REFERENCE FRAMES . . . . . . . . . 0
NUMELQ: NUMBER OF 2D SOLID ELEMENTS . . . . . . . . . 0
NUMELS: NUMBER OF 3D SOLID ELEMENTS . . . . . . . . . 0
NUMELC: NUMBER OF 3D SHELL ELEMENTS (4-NODES) . . . . 29402
NUMELT: NUMBER OF 3D TRUSS ELEMENTS . . . . . . . . . 0
NUMELP: NUMBER OF 3D BEAM ELEMENTS . . . . . . . . . 0
NUMELR: NUMBER OF 3D SPRING ELEMENTS. . . . . . . . . 160
NUMELTG: NUMBER OF 3D SHELL ELEMENTS (3-NODES). . . . 580
NUMELX: NUMBER OF MULTIPURPOSE ELEMENTS . . . . . . . 0
NUMSPH : NUMBER OF SMOOTH PARTICLES (SPH CELLS) . . . 0
NSPHBCS: NUMBER OF SPH SYMETRY CONDITIONS . . . . . . 0
NSPHIO : NUMBER OF SPH INLET/OUTLET CONDITIONS. . . . 0

NFUNCT: NUMBER OF USER'S FUNCTIONS. . . . . . . . . . 2
NGRAV: NUMBER OF GRAVITY LOADS . . . . . . . . . . . 0
NCONLD: NUMBER OF CONCENTRATED LOADS. . . . . . . . . 2
NINVEL: NUMBER OF INITIAL VELOCITIES. . . . . . . . . 0
NPRELD: NUMBER OF PRESSURE LOADS. . . . . . . . . . . 0
NUMBER OF ACCELEROMETERS. . . . . . . . . . . . . . . 0
NUMBER OF SENSORS . . . . . . . . . . . . . . . . . . 0
NUMBER OF GAUGES. . . . . . . . . . . . . . . . . . . 0
NINTER: NUMBER OF INTERFACES. . . . . . . . . . . . . 2
NRWALL: NUMBER OF RIGID WALLS . . . . . . . . . . . . 0
NRBODY: NUMBER OF RIGID BODIES. . . . . . . . . . . . 8
NFXBODY: NUMBER OF FLEXIBLE BODIES. . . . . . . . . . 0
NCONX : NUMBER OF RIGID LINKS TO MADYMO BODIES. . . . 0
NODMAS: NUMBER OF ADDED NODAL MASSES. . . . . . . . . 0
NIMPDISP: NUMBER OF IMPOSED DISPLACEMENTS . . . . . . 0
NIMPVEL: NUMBER OF IMPOSED VELOCITIES . . . . . . . . 0
NIMPACC: NUMBER OF IMPOSED ACCELERATIONS . . . . . . 0
NRIVET: NUMBER OF RIVETS OR SPOT WELDS. . . . . . . . 0
NSECT : NUMBER OF SECTIONS SAVED (TIME HISTORY PLOTS) 0
NJOINT: NUMBER OF JOINTS. . . . . . . . . . . . . . . 0
NACTIV: NUMBER OF ELEMENT DESACTIVATION GROUPS. . . . 0
NDAMP: NUMBER OF RAYLEIGH DAMPING GROUPS . . . . . . 0
NGJOINT: NUMBER OF GEAR TYPE JOINTS . . . . . . . . . 0
NUMMPC: NUMBER OF MULTI-POINT CONSTRAINTS . . . . . . 0
NR2RLNK: NUMBER OF EXTERNAL COUPLING LINKS . . . . . 0
NSUBDOM: NUMBER OF SUBDOMAINS . . . . . .. . . . . . 0
NVOLU: NUMBER OF MONITORED VOLUMES . . . . . . . . . 0
NEIG: NUMBER OF EIGEN AND STATIC MODES PROBLEMS . . 0
NGRAPH: GRAPH DEFINITION FOR MULT-LEVEL CONDENSATION. 0
NBEM: NUMBER OF BEM SOLVED PROBLEMS . . . . . . . . 0
NRBE2: NUMBER OF RBE2 RIGID ELEMENTS . . . . . . . . 0
NRBE3: NUMBER OF RBE3 CONSTRAINT ELEMENTS . . . . . 0
INITIAL STRESS FILE =
FLAG ISIGI. . . 0

N2D3D : ANALYSIS TYPE: 0=3D,1=AXISYM,2=PLANE STRAIN . 0

ANALYSIS OPTIONS
----------------

INTEG8: 8 GAUSS POINT CONDENSED INTEGRATION . . . . . 0
IPARITH: PARALLEL ARITHMETIC FLAG (2 OFF, 1 0N) . . . 1
ISUB : (OLD) SUBCYCLING (1:YES 0:NO) . . . . . . . . 0
MSHSUB: MEMORY ALLOCATION FOR (NEW) SHELLS SUBCYCLING
(1:YES 0:NO). . . 0
IUSERW: GENERAL USER WINDOW FLAG. . . . . . . . . . . 0
ISOLID: DEFAULT BRICK FORMULATION FLAG. . . . . . . . 1
ISST_S: DEFAULT BRICK SMALL STRAIN FLAG . . . . . . . 0
IPLA_S: DEFAULT SOLID STRESS PLASTICITY FLAG. . . . . 2
ISHELL: DEFAULT SHELL FORMULATION FLAG. . . . . . . . 1
ISST : DEFAULT SHELL SMALL STRAIN FLAG . . . . . . . 0
ITHK : DEFAULT SHELL THICKNESS VARIATION FLAG. . . . 0
IPLA : DEFAULT PLANE STRESS PLASTICITY FLAG. . . . . 0
ISTR : DEFAULT SHELL STRAIN COMPUTATION FLAG . . . . 0
ISHEA : DEFAULT SHELL SHEAR COMPUTATION FLAG. . . . . 0
INSH : SHELL INERTIA FLAG. . . . . . . . . . . . . . 0
ISH3N : DEFAULT 3 NODE SHELL FORMULATION FLAG . . . . 2
NPTS : SHELL PROPERTIES DEFAULT NUMBER OF
INTEGRATION POINTS OR LAYERS. . . . . . . . . 0
ISTRA : DEFAULT SOLID STRAIN COMPUTATION FLAG . . . . 2

ISHFRAM:LOCAL SHELL FRAME DEFINITION. . . . . . . . . 0

LAGRANGE MULTIPLIER OPTIONS
---------------------------
LAGM_TOL:CONVERGENCE CRITERIUM. . . . . . . . . . . . 1.0000000000000E-11

NODAL MASS DISTRIBUTION FLAG . . . . . . . . . 0

SPEED PARAMETERS
----------------

STARTER RUNNING ON. . . . . . . . . . . . . . . . . . 1 THREAD
NUMBER OF SPMD DOMAINS. . . . . . . . . . . . . . . . 1
NUMBER OF THREADS PER DOMAIN. . . . . . . . . . . . . 1
ARCHITECTURE OPTIMIZATION . . . . . . . . . . . . . . 22, win64
SIZE OF ELEMENT BUFFER. . . . . . . . . . . . . . . . 128

UNIT SYSTEMS DEFINITION
-----------------------

MASS LENGTH TIME
WORK UNIT SYSTEM . . . . . . ( N.A, N.A, N.A ) 1.0000000000000E+00 1.0000000000000E+00 1.0000000000000E+00
INPUT UNIT SYSTEM . . . . . ( N.A, N.A, N.A ) 1.0000000000000E+00 1.0000000000000E+00 1.0000000000000E+00

LOAD CURVES
-----------
NUMBER OF LOAD CURVES. . . . . . . . = 2

LOAD CURVE ID . . . . . . . . . . . = 1

X Y
0.000000000000 1333.330000000
0.1000000000000 1333.330000000
0.2000000000000 1333.330000000

LOAD CURVE ID . . . . . . . . . . . = 2

X Y
0.000000000000 4000.000000000
0.1000000000000 4000.000000000
0.2000000000000 4000.000000000

TABLES
------
NUMBER OF TABLES . . . . . . . . . . = 0

FUNCTION TRANSFORMATION

steel
MATERIAL NUMBER . . . . . . . . . . . .= 1
MATERIAL LAW. . . . . . . . . . . . . .= 2

INITIAL DENSITY . . . . . . . . . . . .= 7.8000000000000E-09
EOS REFERENCE DENSITY . . . . . . . . .= 7.8000000000000E-09

ELASTIC PLASTIC LAW
-------------------

YOUNG'S MODULUS . . . . . . . . . . . .= 210000.0000000
POISSON'S RATIO . . . . . . . . . . . .= 0.3000000000000
SHEAR MODULUS . . . . . . . . . . . . .= 80769.23076923

JOHNSON COOK MODEL :
YIELD COEFFICIENT A . . . . . . . . . .= 310.0000000000
YIELD COEFFICIENT B . . . . . . . . . .= 350.0000000000
YIELD COEFFICIENT N . . . . . . . . . .= 0.5000000000000
EPS-MAX . . . . . . . . . . . . . . . .= 1.0000000000000E+30
SIG-MAX . . . . . . . . . . . . . . . .= 440.0000000000
ISO-KINEMATIC HARDENNING FACTOR. . . . = 0.000000000000

STRAIN RATE COEFFICIENT CC. . . . . . .= 0.000000000000
REFERENCE STRAIN RATE . . . . . . . . .= 1.000000000000
FLAG FOR STRAIN RATE ON SIG-MAX . . . .= 1
SMOOTH STRAIN RATE OPTION . . . . . . .= 1
STRAIN RATE CUTTING FREQUENCY . . . . .= 1.0000000000000E+30
TEMPERATURE EXPONENT. . . . . . . . . .= 1.000000000000
MELTING TEMPERATURE K . . . . . . . . .= 1.0000000000000E+30
SPECIFIC HEAT Rho*Cp. . . . . . . . . .= 0.000000000000
INITIAL TEMPERATURE K . . . . . . . . .= 298.0000000000

material1
MATERIAL NUMBER . . . . . . . . . . . .= 2
MATERIAL LAW. . . . . . . . . . . . . .= 13

INITIAL DENSITY . . . . . . . . . . . .= 3.5000000000000E-09
EOS REFERENCE DENSITY . . . . . . . . .= 3.5000000000000E-09

RIGID LAW ,/ -----------

YOUNG'S MODULUS . . . . . . . . . . . .= 0.1050E+07
POISSON'S RATIO . . . . . . . . . . . .= 0.1000E+00
SHEAR MODULUS . . . . . . . . . . . . .= 0.4773E+06

PROPERTY SETS
-------------

steeltube
ISOTROPIC SHELL PROPERTY SET
PROPERTY SET NUMBER . . . . . . . . . .= 1
NUMBER OF INTEGRATION POINTS. . . . . .= 0
POST PROCESSING STRAIN FLAG . . . . . .= 0
SHELL THICKNESS . . . . . . . . . . . .= 1.500000000000
SMALL STRAIN FLAG . . . . . . . . . . .= 2
SHELL FORMULATION FLAG. . . . . . . . .= 1
3NODE SHELL FORMULATION FLAG. . . . . .= 2
DRILLING D.O.F. FLAG . . . . . . . . .= 0
SHELL MEMBRANE DAMPING. . . . . . . . .= 0.000000000000
SHELL NUMERICAL DAMPING . . . . . . . .= 1.0000000000000E-02
SHEAR AREA REDUCTION FACTOR . . . . . .= 0.8333333333333
SHEAR FORMULATION FLAG. . . . . . . . .= 0
THICKNESS VARIATION FLAG. . . . . . . .= 0
PLASTICITY FORMULATION FLAG . . . . . .= 0

prop3mm
ISOTROPIC SHELL PROPERTY SET
PROPERTY SET NUMBER . . . . . . . . . .= 2
NUMBER OF INTEGRATION POINTS. . . . . .= 0
POST PROCESSING STRAIN FLAG . . . . . .= 0
SHELL THICKNESS . . . . . . . . . . . .= 3.000000000000
SMALL STRAIN FLAG . . . . . . . . . . .= 2
SHELL FORMULATION FLAG. . . . . . . . .= 1
3NODE SHELL FORMULATION FLAG. . . . . .= 2
DRILLING D.O.F. FLAG . . . . . . . . .= 0
SHELL MEMBRANE DAMPING. . . . . . . . .= 0.000000000000
SHELL NUMERICAL DAMPING . . . . . . . .= 1.0000000000000E-02
SHEAR AREA REDUCTION FACTOR . . . . . .= 0.8333333333333
SHEAR FORMULATION FLAG. . . . . . . . .= 0
THICKNESS VARIATION FLAG. . . . . . . .= 0
PLASTICITY FORMULATION FLAG . . . . . .= 0

prop5mm
ISOTROPIC SHELL PROPERTY SET
PROPERTY SET NUMBER . . . . . . . . . .= 3
NUMBER OF INTEGRATION POINTS. . . . . .= 0
POST PROCESSING STRAIN FLAG . . . . . .= 0
SHELL THICKNESS . . . . . . . . . . . .= 5.000000000000
SMALL STRAIN FLAG . . . . . . . . . . .= 2
SHELL FORMULATION FLAG. . . . . . . . .= 1
3NODE SHELL FORMULATION FLAG. . . . . .= 2
DRILLING D.O.F. FLAG . . . . . . . . .= 0
SHELL MEMBRANE DAMPING. . . . . . . . .= 0.000000000000
SHELL NUMERICAL DAMPING . . . . . . . .= 1.0000000000000E-02
SHEAR AREA REDUCTION FACTOR . . . . . .= 0.8333333333333
SHEAR FORMULATION FLAG. . . . . . . . .= 0
THICKNESS VARIATION FLAG. . . . . . . .= 0
PLASTICITY FORMULATION FLAG . . . . . .= 0

prop1mm
ISOTROPIC SHELL PROPERTY SET
PROPERTY SET NUMBER . . . . . . . . . .= 4
NUMBER OF INTEGRATION POINTS. . . . . .= 0
POST PROCESSING STRAIN FLAG . . . . . .= 0
SHELL THICKNESS . . . . . . . . . . . .= 1.000000000000
SMALL STRAIN FLAG . . . . . . . . . . .= 2
SHELL FORMULATION FLAG. . . . . . . . .= 1
3NODE SHELL FORMULATION FLAG. . . . . .= 2
DRILLING D.O.F. FLAG . . . . . . . . .= 0
SHELL MEMBRANE DAMPING. . . . . . . . .= 0.000000000000
SHELL NUMERICAL DAMPING . . . . . . . .= 1.0000000000000E-02
SHEAR AREA REDUCTION FACTOR . . . . . .= 0.8333333333333
SHEAR FORMULATION FLAG. . . . . . . . .= 0
THICKNESS VARIATION FLAG. . . . . . . .= 0
PLASTICITY FORMULATION FLAG . . . . . .= 0

property1
SPRING PROPERTY SET
PROPERTY SET NUMBER . . . . . . . . . .= 5
SPRING MASS . . . . . . . . . . . . . .= 1.0000000000000E-06
SPRING INERTIA. . . . . . . . . . . . .= 1.0000000000000E-04
SKEW FRAME NUMBER (0:GLOBAL). . . . . .= 0
SENSOR NUMBER (0:NOT USED). . . . . . .= 0
SENSOR FLAG (0:ACTIV 1:DISACT 2:BOTH) .= 0
FAILURE FLAG (0:UNCOUPLED 1:COUPLED). .= 0
FAILURE CRITERIUM (DISPL/FORCE/ENERGY).= 0
1:DISPLACEMENT 2:FORCE 3:ENERGY

X TRANSLATION
SPRING STIFFNESS. . . . . . . . . . . .= 1000000.000000
SPRING DAMPING. . . . . . . . . . . . .= 0.000000000000
FORCE/DISPL. CURVE NUMBER . . . . . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
FORCE/DISPL. CURVE NUMBER 2 (H=4) . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
HARDENING FLAG H. . . . . . . . . . . .= 0
0:ELASTIC 1:ISOTROPIC 2:UNCOUPLED
4:KINEMATIC 5:UNCOUPLED NL (UN/RE)LOADING
DYNAMIC AMPLIFICATION FACTOR A. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR B. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR D. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR E. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR IGF3 . . .= 1.000000000000
DYNAMIC AMPLIFICATION CURVE NUMBER. . .= 0
DYNAMIC AMPLIFICATION CURVE 2 NUMBER. .= 0
NEGATIVE FAILURE DISPLACEMENT . . . . .=-1.0000000000000E+30
POSITIVE FAILURE DISPLACEMENT . . . . .= 1.0000000000000E+30

Y TRANSLATION
SPRING STIFFNESS. . . . . . . . . . . .= 1000000.000000
SPRING DAMPING. . . . . . . . . . . . .= 0.000000000000
FORCE/DISPL. CURVE NUMBER . . . . . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
FORCE/DISPL. CURVE NUMBER 2 (H=4) . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
HARDENING FLAG H. . . . . . . . . . . .= 0
0:ELASTIC 1:ISOTROPIC 2:UNCOUPLED
4:KINEMATIC 5:UNCOUPLED NL (UN/RE)LOADING
DYNAMIC AMPLIFICATION FACTOR A. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR B. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR D. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR E. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR IGF3 . . .= 1.000000000000
DYNAMIC AMPLIFICATION CURVE NUMBER. . .= 0
DYNAMIC AMPLIFICATION CURVE 2 NUMBER. .= 0
NEGATIVE FAILURE DISPLACEMENT . . . . .=-1.0000000000000E+30
POSITIVE FAILURE DISPLACEMENT . . . . .= 1.0000000000000E+30

Z TRANSLATION
SPRING STIFFNESS. . . . . . . . . . . .= 1000000.000000
SPRING DAMPING. . . . . . . . . . . . .= 0.000000000000
FORCE/DISPL. CURVE NUMBER . . . . . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
FORCE/DISPL. CURVE NUMBER 2 (H=4) . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
HARDENING FLAG H. . . . . . . . . . . .= 0
0:ELASTIC 1:ISOTROPIC 2:UNCOUPLED
4:KINEMATIC 5:UNCOUPLED NL (UN/RE)LOADING
DYNAMIC AMPLIFICATION FACTOR A. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR B. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR D. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR E. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR IGF3 . . .= 1.000000000000
DYNAMIC AMPLIFICATION CURVE NUMBER. . .= 0
DYNAMIC AMPLIFICATION CURVE 2 NUMBER. .= 0
NEGATIVE FAILURE DISPLACEMENT . . . . .=-1.0000000000000E+30
POSITIVE FAILURE DISPLACEMENT . . . . .= 1.0000000000000E+30

X ROTATION
SPRING STIFFNESS. . . . . . . . . . . .= 1000000.000000
SPRING DAMPING. . . . . . . . . . . . .= 0.000000000000
MOMENT/ROTATION CURVE NUMBER. . . . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
MOMENT/ROTATION CURVE NUMBER 2 (H=4). .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
HARDENING FLAG H. . . . . . . . . . . .= 0
0:ELASTIC 1:ISOTROPIC 2:UNCOUPLED
4:KINEMATIC 5:UNCOUPLED NL (UN/RE)LOADING
DYNAMIC AMPLIFICATION FACTOR A. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR B. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR D. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR E. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR IGF3 . . .= 1.000000000000
DYNAMIC AMPLIFICATION CURVE NUMBER. . .= 0
DYNAMIC AMPLIFICATION CURVE 2 NUMBER. .= 0
NEGATIVE FAILURE ROTATION . . . . . . .=-1.0000000000000E+30
POSITIVE FAILURE ROTATION . . . . . . .= 1.0000000000000E+30

Y ROTATION
SPRING STIFFNESS. . . . . . . . . . . .= 1000000.000000
SPRING DAMPING. . . . . . . . . . . . .= 0.000000000000
MOMENT/ROTATION CURVE NUMBER. . . . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
MOMENT/ROTATION CURVE NUMBER 2 (H=4). .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
HARDENING FLAG H. . . . . . . . . . . .= 0
0:ELASTIC 1:ISOTROPIC 2:UNCOUPLED
4:KINEMATIC 5:UNCOUPLED NL (UN/RE)LOADING
DYNAMIC AMPLIFICATION FACTOR A. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR B. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR D. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR E. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR IGF3 . . .= 1.000000000000
DYNAMIC AMPLIFICATION CURVE NUMBER. . .= 0
DYNAMIC AMPLIFICATION CURVE 2 NUMBER. .= 0
NEGATIVE FAILURE ROTATION . . . . . . .=-1.0000000000000E+30
POSITIVE FAILURE ROTATION . . . . . . .= 1.0000000000000E+30

Z ROTATION
SPRING STIFFNESS. . . . . . . . . . . .= 1000000.000000
SPRING DAMPING. . . . . . . . . . . . .= 0.000000000000
MOMENT/ROTATION CURVE NUMBER. . . . . .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
MOMENT/ROTATION CURVE NUMBER 2 (H=4). .= 0
ABSCISSA SCALE FACTOR ON CURVE . . . . = 1.000000000000
HARDENING FLAG H. . . . . . . . . . . .= 0
0:ELASTIC 1:ISOTROPIC 2:UNCOUPLED
4:KINEMATIC 5:UNCOUPLED NL (UN/RE)LOADING
DYNAMIC AMPLIFICATION FACTOR A. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR B. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR D. . . . .= 1.000000000000
DYNAMIC AMPLIFICATION FACTOR E. . . . .= 0.000000000000
DYNAMIC AMPLIFICATION FACTOR IGF3 . . .= 1.000000000000
DYNAMIC AMPLIFICATION CURVE NUMBER. . .= 0
DYNAMIC AMPLIFICATION CURVE 2 NUMBER. .= 0
NEGATIVE FAILURE ROTATION . . . . . . .=-1.0000000000000E+30
POSITIVE FAILURE ROTATION . . . . . . .= 1.0000000000000E+30

SMOOTH STRAIN RATE OPTION . . .. . . . = 0
STRAIN RATE CUTTING FREQUENCY .. . . .= 0.000000000000

PARTS
-----

PART: 66,Steeltube_mid
----
PROPERTY: 1,steeltube
MATERIAL: 1,steel
SUBSET : 0
VIRT. THICKN: 0.000000000000

PART: 67,clamps_mid
----
PROPERTY: 3,prop5mm
MATERIAL: 1,steel
SUBSET : 0
VIRT. THICKN: 0.000000000000

PART: 68,gusset_clamp
----
PROPERTY: 2,prop3mm
MATERIAL: 1,steel
SUBSET : 0
VIRT. THICKN: 0.000000000000

PART: 69,backplate_mid
----
PROPERTY: 4,prop1mm
MATERIAL: 1,steel
SUBSET : 0
VIRT. THICKN: 0.000000000000

PART: 70,flange5mm_mid
----
PROPERTY: 3,prop5mm
MATERIAL: 1,steel

RAMGANESH · May 2016

Dear Rahul,

My model is error free and warning free.but the results are seem to be different.kindly give your suggestions.

Thanks

Ram

Rahul Rajan_21763 · May 2016

could you try runing by changing the Cload?If possible share h3d & t01 file.

RAMGANESH · May 2016

Dear Rahul,

I had shared the files in your dropbox

Thanks

Ram

Altair Forum User · May 2016

Hi Ram,

Consider increasing the thickness of the below shown in the image or reduce the load.

Maybe you can do a optimization.

<?xml version="1.0" encoding="UTF-8"?>

RAMGANESH · May 2016

Dear Prakash ,

I had made the design change in that gusset and got the expected results.

Thanks for the valuable support.

Thanks

Ram

Rahul Rajan_21763 · May 2016

Thanks for the update Ram.

Altair Forum User · May 2016

Altair Forum User said:

Dear Prakash ,

I had made the design change in that gusset and got the expected results.

Thanks for the valuable support.

No Problem /emoticons/default_smile.png' srcset='/emoticons/smile@2x.png 2x' title=':)' width='20'>

Error in output results.

Answers

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