abaqus计算报错CONTACT FORCE ERROR TOLERANCE FOR CONVERT SDI=YES
OMPATIBILITY ERRORS:
TYPE NUMBER EXCEEDING TOLERANCE MAXIMUM ERROR IN ELEMENT
COUPLING DISPLACEMENT 0 -4.777E-14 513
COUPLING ROTATION 0 -1.562E-14 4011
NUMBER OF EQUATIONS = 971582 NUMBER OF FLOATING PT. OPERATIONS = 2.56E+11
USING THE DIRECT SOLVER WITH 4 PROCESSORS
CHECK POINT START OF SOLVER
CHECK POINT END OF SOLVER
ELAPSED USER TIME (SEC) = 49.400
ELAPSED SYSTEM TIME (SEC) = 1.5000
ELAPSED TOTAL CPU TIME (SEC) = 50.900
ELAPSED WALLCLOCK TIME (SEC) = 32
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 2 RATIO = 939.902E+09 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 3 RATIO = 240.222E+09 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 2
AVERAGE FORCE 4.444E-09 TIME AVG. FORCE 1.000E-02
LARGEST RESIDUAL FORCE -4.397E-06 AT NODE 10228 DOF 1
LARGEST INCREMENT OF DISP. 4.710E-09 AT NODE 11327507 DOF 2
LARGEST CORRECTION TO DISP. 3.379E-09 AT NODE 11327507 DOF 2
THE FORCE IS ZERO EVERYWHERE BUT THE FORCE RESIDUAL OR
THE DISP. CORRECTION IS NON-ZERO
AVERAGE MOMENT 1.842E-09 TIME AVG. MOMENT 4.975E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT 1.619E-05 AT NODE 11325831 DOF 6
LARGEST INCREMENT OF ROTATION -4.453E-12 AT NODE 11383417 DOF 6
LARGEST CORRECTION TO ROTATION -3.725E-12 AT NODE 11383417 DOF 6
ALL ROTATION CORRECTIONS ARE ZERO
COMPATIBILITY ERRORS:
TYPE NUMBER EXCEEDING TOLERANCE MAXIMUM ERROR IN ELEMENT
COUPLING DISPLACEMENT 0 8.645E-14 513
COUPLING ROTATION 0 -2.259E-14 513
NUMBER OF EQUATIONS = 971582 NUMBER OF FLOATING PT. OPERATIONS = 2.56E+11
USING THE DIRECT SOLVER WITH 4 PROCESSORS
CHECK POINT START OF SOLVER
CHECK POINT END OF SOLVER
ELAPSED USER TIME (SEC) = 42.200
ELAPSED SYSTEM TIME (SEC) = 0.50000
ELAPSED TOTAL CPU TIME (SEC) = 42.700
ELAPSED WALLCLOCK TIME (SEC) = 27
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 2 RATIO = 1.25864E+12.
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 3 RATIO = 41.7608E+09 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 6 RATIO = 42.8605E+09 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 3
AVERAGE FORCE 4.605E-09 TIME AVG. FORCE 1.000E-02
LARGEST RESIDUAL FORCE 4.331E-06 AT NODE 10248 DOF 1
LARGEST INCREMENT OF DISP. 6.692E-09 AT NODE 11327507 DOF 2
LARGEST CORRECTION TO DISP. -2.483E-09 AT NODE 11378816 DOF 1
THE FORCE IS ZERO EVERYWHERE BUT THE FORCE RESIDUAL OR
THE DISP. CORRECTION IS NON-ZERO
AVERAGE MOMENT 1.964E-09 TIME AVG. MOMENT 4.975E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -5.987E-06 AT NODE 11325831 DOF 6
LARGEST INCREMENT OF ROTATION -5.366E-12 AT NODE 11441714 DOF 6
LARGEST CORRECTION TO ROTATION -1.218E-12 AT NODE 11397217 DOF 6
ALL ROTATION CORRECTIONS ARE ZERO
COMPATIBILITY ERRORS:
TYPE NUMBER EXCEEDING TOLERANCE MAXIMUM ERROR IN ELEMENT
COUPLING DISPLACEMENT 0 -6.607E-14 513
COUPLING ROTATION 0 1.890E-14 4023
NUMBER OF EQUATIONS = 971582 NUMBER OF FLOATING PT. OPERATIONS = 2.56E+11
USING THE DIRECT SOLVER WITH 4 PROCESSORS
CHECK POINT START OF SOLVER
CHECK POINT END OF SOLVER
ELAPSED USER TIME (SEC) = 43.700
ELAPSED SYSTEM TIME (SEC) = 0.50000
ELAPSED TOTAL CPU TIME (SEC) = 44.200
ELAPSED WALLCLOCK TIME (SEC) = 27
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 2 RATIO = 605.432E+09 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 3 RATIO = 38.5673E+09 .
***WARNING: SOLVER PROBLEM. NUMERICAL SINGULARITY WHEN PROCESSING NODE
11180271 D.O.F. 6 RATIO = 29.7909E+09 .
CONVERGENCE CHECKS FOR EQUILIBRIUM ITERATION 4
AVERAGE FORCE 4.703E-09 TIME AVG. FORCE 1.000E-02
LARGEST RESIDUAL FORCE 5.886E-06 AT NODE 10246 DOF 1
LARGEST INCREMENT OF DISP. -3.250E-09 AT NODE 11378820 DOF 1
LARGEST CORRECTION TO DISP. -4.558E-09 AT NODE 11327507 DOF 2
THE FORCE IS ZERO EVERYWHERE BUT THE FORCE RESIDUAL OR
THE DISP. CORRECTION IS NON-ZERO
AVERAGE MOMENT 2.042E-09 TIME AVG. MOMENT 4.975E-02
(FROM FORCE FIELD)
LARGEST RESIDUAL MOMENT -1.876E-05 AT NODE 11325831 DOF 5
LARGEST INCREMENT OF ROTATION -4.100E-12 AT NODE 11410522 DOF 6
LARGEST CORRECTION TO ROTATION 1.615E-12 AT NODE 11423022 DOF 6
ALL ROTATION CORRECTIONS ARE ZERO