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Abaqus 3DEXPERIENCE R2017x Date 03-12月-2020 Time 19:04:29
For use by Supplied by Team-SolidSQUAD under license from Dassault Systemes or its subsidiary.
Exhaust manifold heat transfer
Co-simulation of Hot Exhaust Gases in the Manifold
STEP 1 INCREMENT 1 STEP TIME 0.00
S T E P 1 T R A N S I E N T H E A T T R A N S F E R
Co-simulation of Hot Exhaust Gases in the Manifold
FIXED TIME INCREMENTS
TIME INCREMENT IS 250.
TIME PERIOD IS 1.000E+04
CONVERGENCE TOLERANCE PARAMETERS FOR HEAT FLUX
CRITERION FOR RESIDUAL HEAT FLUX FOR A NONLINEAR PROBLEM 5.000E-03
CRITERION FOR TEMP. CORRECTION IN A NONLINEAR PROBLEM 1.000E-02
INITIAL VALUE OF TIME AVERAGE HEAT FLUX 1.000E-02
AVERAGE HEAT FLUX IS TIME AVERAGE HEAT FLUX
ALTERNATE CRIT. FOR RESIDUAL HEAT FLUX FOR A NONLINEAR PROBLEM 2.000E-02
CRITERION FOR ZERO HEAT FLUX RELATIVE TO TIME AVRG. HEAT FLUX 1.000E-05
CRITERION FOR RESIDUAL HEAT FLUX WHEN THERE IS ZERO FLUX 1.000E-05
CRITERION FOR TEMP. CORRECTION WHEN THERE IS ZERO FLUX 1.000E-03
CRITERION FOR RESIDUAL HEAT FLUX FOR A LINEAR INCREMENT 1.000E-08
FIELD CONVERSION RATIO 1.00
CRITERION FOR ZERO HEAT FLUX REL. TO TIME AVRG. MAX. HEAT FLUX 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
ITERATION CONTROL PARAMETERS:
FIRST EQUILIBRIUM ITERATION FOR CONSECUTIVE DIVERGENCE CHECK 4
EQUILIBRIUM ITERATION AFTER WHICH ALTERNATE RESIDUAL IS USED 9
MAXIMUM EQUILIBRIUM ITERATIONS ALLOWED 16
MAXIMUM ITERATIONS FOR SEVERE DISCONTINUITIES 12
GLOBAL STABILIZATION CONTROL IS NOT USED
PRINT OF INCREMENT NUMBER, TIME, ETC., EVERY 1 INCREMENTS
THE MAXIMUM NUMBER OF INCREMENTS IN THIS STEP IS 2000
LINEAR EXTRAPOLATION WILL BE USED
CHARACTERISTIC ELEMENT LENGTH 6.637E-03
DETAILS REGARDING ACTUAL SOLUTION WAVEFRONT REQUESTED
DETAILED OUTPUT OF DIAGNOSTICS TO DATABASE REQUESTED
PRINT OF INCREMENT NUMBER, TIME, ETC., TO THE MESSAGE FILE EVERY 1 INCREMENTS
COLLECTING MODEL CONSTRAINT INFORMATION FOR OVERCONSTRAINT CHECKS
COLLECTING STEP CONSTRAINT INFORMATION FOR OVERCONSTRAINT CHECKS
THIS IS A CO-SIMULATION STEP
Abaqus MAY TAKE ONE OR MORE INCREMENTS FOR EACH COUPLING STEP
***NOTE: Abaqus/Standard has received the following message from the
co-simulation engine:
Director terminated the analysis due to early termination by a client. Please check for errors for each of the analysis involved in co-simulation and also verify that the co-simulation duration time specified in the configuration file is correct.
***ERROR: Due to this co-simulation Failure Abaqus cannot continue.
ANALYSIS SUMMARY:
TOTAL OF 0 INCREMENTS
0 CUTBACKS IN AUTOMATIC INCREMENTATION
0 ITERATIONS INCLUDING CONTACT ITERATIONS IF PRESENT
0 PASSES THROUGH THE EQUATION SOLVER OF WHICH
0 INVOLVE MATRIX DECOMPOSITION, INCLUDING
0 DECOMPOSITION(S) OF THE MASS MATRIX
1 REORDERING OF EQUATIONS TO MINIMIZE WAVEFRONT
0 ADDITIONAL RESIDUAL EVALUATIONS FOR LINE SEARCHES
0 ADDITIONAL OPERATOR EVALUATIONS FOR LINE SEARCHES
1 WARNING MESSAGES DURING USER INPUT PROCESSING
0 WARNING MESSAGES DURING ANALYSIS
0 ANALYSIS WARNINGS ARE NUMERICAL PROBLEM MESSAGES
0 ANALYSIS WARNINGS ARE NEGATIVE EIGENVALUE MESSAGES
1 ERROR MESSAGES
JOB TIME SUMMARY
USER TIME (SEC) = 0.70000
SYSTEM TIME (SEC) = 0.0000
TOTAL CPU TIME (SEC) = 0.70000
WALLCLOCK TIME (SEC) = 13
2020年12月03日 11点12分
1
For use by Supplied by Team-SolidSQUAD under license from Dassault Systemes or its subsidiary.
Exhaust manifold heat transfer
Co-simulation of Hot Exhaust Gases in the Manifold
STEP 1 INCREMENT 1 STEP TIME 0.00
S T E P 1 T R A N S I E N T H E A T T R A N S F E R
Co-simulation of Hot Exhaust Gases in the Manifold
FIXED TIME INCREMENTS
TIME INCREMENT IS 250.
TIME PERIOD IS 1.000E+04
CONVERGENCE TOLERANCE PARAMETERS FOR HEAT FLUX
CRITERION FOR RESIDUAL HEAT FLUX FOR A NONLINEAR PROBLEM 5.000E-03
CRITERION FOR TEMP. CORRECTION IN A NONLINEAR PROBLEM 1.000E-02
INITIAL VALUE OF TIME AVERAGE HEAT FLUX 1.000E-02
AVERAGE HEAT FLUX IS TIME AVERAGE HEAT FLUX
ALTERNATE CRIT. FOR RESIDUAL HEAT FLUX FOR A NONLINEAR PROBLEM 2.000E-02
CRITERION FOR ZERO HEAT FLUX RELATIVE TO TIME AVRG. HEAT FLUX 1.000E-05
CRITERION FOR RESIDUAL HEAT FLUX WHEN THERE IS ZERO FLUX 1.000E-05
CRITERION FOR TEMP. CORRECTION WHEN THERE IS ZERO FLUX 1.000E-03
CRITERION FOR RESIDUAL HEAT FLUX FOR A LINEAR INCREMENT 1.000E-08
FIELD CONVERSION RATIO 1.00
CRITERION FOR ZERO HEAT FLUX REL. TO TIME AVRG. MAX. HEAT FLUX 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
ITERATION CONTROL PARAMETERS:
FIRST EQUILIBRIUM ITERATION FOR CONSECUTIVE DIVERGENCE CHECK 4
EQUILIBRIUM ITERATION AFTER WHICH ALTERNATE RESIDUAL IS USED 9
MAXIMUM EQUILIBRIUM ITERATIONS ALLOWED 16
MAXIMUM ITERATIONS FOR SEVERE DISCONTINUITIES 12
GLOBAL STABILIZATION CONTROL IS NOT USED
PRINT OF INCREMENT NUMBER, TIME, ETC., EVERY 1 INCREMENTS
THE MAXIMUM NUMBER OF INCREMENTS IN THIS STEP IS 2000
LINEAR EXTRAPOLATION WILL BE USED
CHARACTERISTIC ELEMENT LENGTH 6.637E-03
DETAILS REGARDING ACTUAL SOLUTION WAVEFRONT REQUESTED
DETAILED OUTPUT OF DIAGNOSTICS TO DATABASE REQUESTED
PRINT OF INCREMENT NUMBER, TIME, ETC., TO THE MESSAGE FILE EVERY 1 INCREMENTS
COLLECTING MODEL CONSTRAINT INFORMATION FOR OVERCONSTRAINT CHECKS
COLLECTING STEP CONSTRAINT INFORMATION FOR OVERCONSTRAINT CHECKS
THIS IS A CO-SIMULATION STEP
Abaqus MAY TAKE ONE OR MORE INCREMENTS FOR EACH COUPLING STEP
***NOTE: Abaqus/Standard has received the following message from the
co-simulation engine:
Director terminated the analysis due to early termination by a client. Please check for errors for each of the analysis involved in co-simulation and also verify that the co-simulation duration time specified in the configuration file is correct.
***ERROR: Due to this co-simulation Failure Abaqus cannot continue.
ANALYSIS SUMMARY:
TOTAL OF 0 INCREMENTS
0 CUTBACKS IN AUTOMATIC INCREMENTATION
0 ITERATIONS INCLUDING CONTACT ITERATIONS IF PRESENT
0 PASSES THROUGH THE EQUATION SOLVER OF WHICH
0 INVOLVE MATRIX DECOMPOSITION, INCLUDING
0 DECOMPOSITION(S) OF THE MASS MATRIX
1 REORDERING OF EQUATIONS TO MINIMIZE WAVEFRONT
0 ADDITIONAL RESIDUAL EVALUATIONS FOR LINE SEARCHES
0 ADDITIONAL OPERATOR EVALUATIONS FOR LINE SEARCHES
1 WARNING MESSAGES DURING USER INPUT PROCESSING
0 WARNING MESSAGES DURING ANALYSIS
0 ANALYSIS WARNINGS ARE NUMERICAL PROBLEM MESSAGES
0 ANALYSIS WARNINGS ARE NEGATIVE EIGENVALUE MESSAGES
1 ERROR MESSAGES
JOB TIME SUMMARY
USER TIME (SEC) = 0.70000
SYSTEM TIME (SEC) = 0.0000
TOTAL CPU TIME (SEC) = 0.70000
WALLCLOCK TIME (SEC) = 13
