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我用tie连接,好像提示自由度没有限制住。 .msg文件如下。 哪位大侠帮忙指点一下啊!多些了!
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1
Abaqus 6.9-3 Date 21-Mar-2010 Time 09:14:22
For use by TEAM TBE under license from Dassault Systemes or its subsidiary.
STEP 1 INCREMENT 1 STEP TIME 0.00
S T E P 1 S T A T I C A N A L Y S I S
AUTOMATIC TIME CONTROL WITH -
A SUGGESTED INITIAL TIME INCREMENT OF 1.00
AND A TOTAL TIME PERIOD OF 1.00
THE MINIMUM TIME INCREMENT ALLOWED IS 1.000E-05
THE MAXIMUM TIME INCREMENT ALLOWED IS 1.00
LINEAR EQUATION SOLVER TYPE DIRECT SPARSE
CONVERGENCE TOLERANCE PARAMETERS FOR FORCE
CRITERION FOR RESIDUAL FORCE FOR A NONLINEAR PROBLEM 5.000E-03
CRITERION FOR DISP. CORRECTION IN A NONLINEAR PROBLEM 1.000E-02
INITIAL VALUE OF TIME AVERAGE FORCE 1.000E-02
AVERAGE FORCE IS TIME AVERAGE FORCE
ALTERNATE CRIT. FOR RESIDUAL FORCE FOR A NONLINEAR PROBLEM 2.000E-02
CRITERION FOR ZERO FORCE RELATIVE TO TIME AVRG. FORCE 1.000E-05
CRITERION FOR RESIDUAL FORCE WHEN THERE IS ZERO FLUX 1.000E-05
CRITERION FOR DISP. CORRECTION WHEN THERE IS ZERO FLUX 1.000E-03
CRITERION FOR RESIDUAL FORCE FOR A LINEAR INCREMENT 1.000E-08
FIELD CONVERSION RATIO 1.00
CRITERION FOR ZERO FORCE REL. TO TIME AVRG. MAX. FORCE 1.000E-05
CRITERION FOR ZERO DISP. RELATIVE TO CHARACTERISTIC LENGTH 1.000E-08
CONVERGENCE TOLERANCE PARAMETERS FOR MOMENT
CRITERION FOR RESIDUAL MOMENT FOR A NONLINEAR PROBLEM 5.000E-03
CRITERION FOR ROTATION CORRECTION IN A NONLINEAR PROBLEM 1.000E-02
INITIAL VALUE OF TIME AVERAGE MOMENT 1.000E-02
AVERAGE MOMENT IS TIME AVERAGE MOMENT
ALTERNATE CRIT. FOR RESIDUAL MOMENT FOR A NONLINEAR PROBLEM 2.000E-02
CRITERION FOR ZERO MOMENT RELATIVE TO TIME AVRG. MOMENT 1.000E-05
CRITERION FOR RESIDUAL MOMENT WHEN THERE IS ZERO FLUX 1.000E-05
CRITERION FOR ROTATION CORRECTION WHEN THERE IS ZERO FLUX 1.000E-03
CRITERION FOR RESIDUAL MOMENT FOR A LINEAR INCREMENT 1.000E-08
FIELD CONVERSION RATIO 1.00
CRITERION FOR ZERO MOMENT REL. TO TIME AVRG. MAX. MOMENT 1.000E-05
VOLUMETRIC STRAIN COMPATIBILITY TOLERANCE FOR HYBRID SOLIDS 1.000E-05
AXIAL STRAIN COMPATIBILITY TOLERANCE FOR HYBRID BEAMS 1.000E-05
TRANS. SHEAR STRAIN COMPATIBILITY TOLERANCE FOR HYBRID BEAMS 1.000E-05
SOFT CONTACT CONSTRAINT COMPATIBILITY TOLERANCE FOR P>P0 5.000E-03
SOFT CONTACT CONSTRAINT COMPATIBILITY TOLERANCE FOR P=0.0 0.100
CONTACT FORCE ERROR TOLERANCE FOR CONVERT SDI=YES 1.00
DISPLACEMENT COMPATIBILITY TOLERANCE FOR DCOUP ELEMENTS 1.000E-05
ROTATION COMPATIBILITY TOLERANCE FOR DCOUP ELEMENTS 1.000E-05
EQUILIBRIUM WILL BE CHECKED FOR SEVERE DISCONTINUITY ITERATIONS
TIME INCREMENTATION CONTROL PARAMETERS:
FIRST EQUILIBRIUM ITERATION FOR CONSECUTIVE DIVERGENCE CHECK 4
EQUILIBRIUM ITERATION AT WHICH LOG. CONVERGENCE RATE CHECK BEGINS 8
EQUILIBRIUM ITERATION AFTER WHICH ALTERNATE RESIDUAL IS USED 9
MAXIMUM EQUILIBRIUM ITERATIONS ALLOWED 16
EQUILIBRIUM ITERATION COUNT FOR CUT-BACK IN NEXT INCREMENT 10
MAXIMUM EQUILIB. ITERS IN TWO INCREMENTS FOR TIME INCREMENT INCREASE 4
MAXIMUM ITERATIONS FOR SEVERE DISCONTINUITIES 50
MAXIMUM CUT-BACKS ALLOWED IN AN INCREMENT 5
MAXIMUM DISCON. ITERS IN TWO INCREMENTS FOR TIME INCREMENT INCREASE 50
MAXIMUM CONTACT AUGMENTATIONS FOR *SURFACE BEHAVIOR,AUGMENTED LAGRANGE 6
CUT-BACK FACTOR AFTER DIVERGENCE 0.2500
CUT-BACK FACTOR FOR TOO SLOW CONVERGENCE 0.5000
CUT-BACK FACTOR AFTER TOO MANY EQUILIBRIUM ITERATIONS 0.7500
CUT-BACK FACTOR AFTER TOO MANY SEVERE DISCONTINUITY ITERATIONS 0.2500
CUT-BACK FACTOR AFTER PROBLEMS IN ELEMENT ASSEMBLY 0.2500
INCREASE FACTOR AFTER TWO INCREMENTS THAT CONVERGE QUICKLY 1.500
MAX. TIME INCREMENT INCREASE FACTOR ALLOWED 1.500
MAX. TIME INCREMENT INCREASE FACTOR ALLOWED (DYNAMICS) 1.250
MAX. TIME INCREMENT INCREASE FACTOR ALLOWED (DIFFUSION) 2.000
MINIMUM TIME INCREMENT RATIO FOR EXTRAPOLATION TO OCCUR 0.1000
MAX. RATIO OF TIME INCREMENT TO STABILITY LIMIT 1.000
FRACTION OF STABILITY LIMIT FOR NEW TIME INCREMENT 0.9500
TIME INCREMENT INCREASE FACTOR BEFORE A TIME POINT 1.000
AUTOMATIC TOLERANCES FOR OVERCLOSURE AND SEPARATION
PRESSURE ARE SUPPRESSED
GLOBAL STABILIZATION CONTROL IS NOT USED
FRICTION IS INCLUDED IN INCREMENT THAT THE CONTACT POINT CLOSES
PRINT OF INCREMENT NUMBER, TIME, ETC., EVERY 1 INCREMENTS
THE MAXIMUM NUMBER OF INCREMENTS IN THIS STEP IS 10000
LINEAR EXTRAPOLATION WILL BE USED
CHARACTERISTIC ELEMENT LENGTH 4.23
DETAILED OUTPUT OF DIAGNOSTICS TO DATABASE REQUESTED
PRINT OF INCREMENT NUMBER, TIME, ETC., TO THE MESSAGE FILE EVERY 1 INCREMENTS
EQUATIONS ARE BEING REORDERED TO MINIMIZE WAVEFRONT
COLLECTING MODEL CONSTRAINT INFORMATION FOR OVERCONSTRAINT CHECKS
COLLECTING STEP CONSTRAINT INFORMATION FOR OVERCONSTRAINT CHECKS
INCREMENT 1 STARTS. ATTEMPT NUMBER 1, TIME INCREMENT 1.00
***WARNING: THERE ARE 2 UNCONNECTED REGIONS IN THE MODEL.
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
IN AN EIGENVALUE EXTRACTION STEP THE NUMBER OF NEGATIVE EIGENVALUES IS
EQUAL TO THE NUMBER OF EIGENVALUES BELOW THE CURRENT SHIFT POINT.
THIS MAY BE USED TO CHECK THAT EIGENVALUES HAVE NOT BEEN MISSED.
NOTE: THE LANCZOS EIGENSOLVER APPLIES AN INTERNAL SHIFT WHICH WILL
RESULT IN NEGATIVE EIGENVALUES.
IN A DIRECT-SOLUTION STEADY-STATE DYNAMIC ANALYSIS, NEGATIVE
EIGENVALUES ARE EXPECTED. A STATIC ANALYSIS CAN BE USED TO VERIFY THAT THE SYSTEM IS STABLE.
IN OTHER CASES, NEGATIVE EIGENVALUES MEAN THAT THE SYSTEM MATRIX IS NOT
POSITIVE DEFINITE:
FOR EXAMPLE, A BIFURCATION (BUCKLING) LOAD MAY HAVE BEEN EXCEEDED.
NEGATIVE EIGENVALUES MAY ALSO OCCUR IF QUADRATIC ELEMENTS ARE
USED TO DEFINE CONTACT SURFACES.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 1
AVERAGE FORCE 3.568E-03 TIME AVG. FORCE 3.568E-03
LARGEST RESIDUAL FORCE 2.80 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 2.822E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 2.822E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -10.8 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -1.365E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -1.365E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 2
AVERAGE FORCE 3.629E-03 TIME AVG. FORCE 3.629E-03
LARGEST RESIDUAL FORCE 2.37 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 5.643E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 2.822E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -19.9 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -2.730E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -1.365E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 3
AVERAGE FORCE 3.709E-03 TIME AVG. FORCE 3.709E-03
LARGEST RESIDUAL FORCE -2.81 AT NODE 244 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 8.465E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 2.822E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -18.0 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -4.094E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -1.365E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 4
AVERAGE FORCE 3.831E-03 TIME AVG. FORCE 3.831E-03
LARGEST RESIDUAL FORCE 2.92 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 1.129E+09 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 2.822E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -33.9 AT NODE 1 DOF 5
INSTANCE:
LARGEST INCREMENT OF ROTATION -5.459E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -1.365E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***NOTE: THE SOLUTION APPEARS TO BE DIVERGING. CONVERGENCE IS JUDGED UNLIKELY.
INCREMENT 1 STARTS. ATTEMPT NUMBER 2, TIME INCREMENT 0.250
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 1
AVERAGE FORCE 8.921E-04 TIME AVG. FORCE 8.921E-04
LARGEST RESIDUAL FORCE 0.700 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 7.054E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 7.054E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -2.70 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -3.412E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -3.412E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 2
AVERAGE FORCE 9.074E-04 TIME AVG. FORCE 9.074E-04
LARGEST RESIDUAL FORCE 0.592 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 1.411E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 7.054E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -4.97 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -6.824E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -3.412E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 3
AVERAGE FORCE 9.272E-04 TIME AVG. FORCE 9.272E-04
LARGEST RESIDUAL FORCE -0.702 AT NODE 244 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 2.116E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 7.054E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -4.50 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -1.024E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -3.412E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 4
AVERAGE FORCE 9.577E-04 TIME AVG. FORCE 9.577E-04
LARGEST RESIDUAL FORCE 0.731 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 2.822E+08 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 7.054E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -8.47 AT NODE 1 DOF 5
INSTANCE:
LARGEST INCREMENT OF ROTATION -1.365E+07 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -3.412E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***NOTE: THE SOLUTION APPEARS TO BE DIVERGING. CONVERGENCE IS JUDGED UNLIKELY.
INCREMENT 1 STARTS. ATTEMPT NUMBER 3, TIME INCREMENT 6.250E-02
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 1
AVERAGE FORCE 2.230E-04 TIME AVG. FORCE 2.230E-04
LARGEST RESIDUAL FORCE 0.175 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 1.764E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 1.764E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -0.676 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -8.530E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -8.530E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 2
AVERAGE FORCE 2.268E-04 TIME AVG. FORCE 2.268E-04
LARGEST RESIDUAL FORCE 0.148 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 3.527E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 1.764E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -1.24 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -1.706E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -8.530E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 3
AVERAGE FORCE 2.318E-04 TIME AVG. FORCE 2.318E-04
LARGEST RESIDUAL FORCE -0.175 AT NODE 244 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 5.291E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 1.764E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -1.13 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -2.559E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -8.530E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 4
AVERAGE FORCE 2.394E-04 TIME AVG. FORCE 2.394E-04
LARGEST RESIDUAL FORCE 0.183 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 7.054E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 1.764E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -2.12 AT NODE 1 DOF 5
INSTANCE:
LARGEST INCREMENT OF ROTATION -3.412E+06 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -8.530E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***NOTE: THE SOLUTION APPEARS TO BE DIVERGING. CONVERGENCE IS JUDGED UNLIKELY.
INCREMENT 1 STARTS. ATTEMPT NUMBER 4, TIME INCREMENT 1.563E-02
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 1
AVERAGE FORCE 5.576E-05 TIME AVG. FORCE 5.576E-05
LARGEST RESIDUAL FORCE 4.375E-02 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 4.409E+06 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 4.409E+06 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -0.169 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -2.132E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -2.132E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 2
AVERAGE FORCE 5.671E-05 TIME AVG. FORCE 5.671E-05
LARGEST RESIDUAL FORCE 3.702E-02 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 8.818E+06 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 4.409E+06 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -0.310 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -4.265E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -2.132E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 3
AVERAGE FORCE 5.795E-05 TIME AVG. FORCE 5.795E-05
LARGEST RESIDUAL FORCE -4.386E-02 AT NODE 244 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 1.323E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 4.409E+06 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -0.281 AT NODE 1 DOF 4
INSTANCE:
LARGEST INCREMENT OF ROTATION -6.397E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -2.132E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
***WARNING: THE SYSTEM MATRIX HAS 1 NEGATIVE EIGENVALUES.
EXPLANATIONS ARE SUGGESTED AFTER THE FIRST OCCURRENCE OF THIS MESSAGE.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.187 D.O.F. 2 RATIO = 3.03274E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 1 RATIO = 43.1192E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 2 RATIO = 20.8326E+12 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
N800-1-1-1.186 D.O.F. 3 RATIO = 22.3203E+12 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 4
AVERAGE FORCE 5.986E-05 TIME AVG. FORCE 5.986E-05
LARGEST RESIDUAL FORCE 4.569E-02 AT NODE 243 DOF 3
INSTANCE: N800-1-1-1
LARGEST INCREMENT OF DISP. 1.764E+07 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
LARGEST CORRECTION TO DISP. 4.409E+06 AT NODE 36 DOF 2
INSTANCE: N800-1-1-1
FORCE EQUILIBRIUM NOT ACHIEVED WITHIN TOLERANCE.
AVERAGE MOMENT 0.00 TIME AVG. MOMENT 4.229E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -0.529 AT NODE 1 DOF 5
INSTANCE:
LARGEST INCREMENT OF ROTATION -8.530E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
LARGEST CORRECTION TO ROTATION -2.132E+05 AT NODE 1 DOF 6
INSTANCE: {assembly node}
THE MOMENT IS ZERO EVERYWHERE BUT THE MOMENT RESIDUAL OR
THE ROTATION CORRECTION IS NON-ZERO
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