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TenBarArea.dat
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1
Abaqus 6.14-4 Date 02-Nov-2017 Time 11:45:19
For use at UNIVERSITY OF FLORIDA under license from Dassault Systemes or its subsidiary.
The Abaqus Software is a product of:
Dassault Systemes SIMULIA Corp.
1301 Atwood Avenue, Suite 101W
Johnston, RI 02919, USA
Available for internal use at UNIVERSITY OF FLORIDA.
The Abaqus Online Support System is accessible
through the "My Support" section of the SIMULIA
Home Page at http://www.simulia.com.
Support policies for academic licenses are described
on the SIMULIA web site at
http://www.3ds.com/products/simulia/academics/
On machine Asteria
you are authorized to run
Abaqus/Standard until 30-Sep-2018
Your site id is: 200000000001545
For assistance or any other information you may
obtain contact information for your local office
from the world wide web at:
http://www.3ds.com/products/simulia/locations/
* * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
* *
* ***************** *
* * N O T I C E * *
* ***************** *
* *
* *
* Abaqus 6.14-4 *
* *
* BUILD ID: 2015_06_11-16.39.29 135079 *
* *
* *
* Please make sure you are using release 6.14 manuals *
* plus the notes accompanying this release. *
* *
* *
* *
* *
* *
* This program may not be used for commercial purposes *
* without payment of a commercial fee. *
* *
* * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
PROCESSING PART, INSTANCE, AND ASSEMBLY INFORMATION
*******************************************************
END PROCESSING PART, INSTANCE, AND ASSEMBLY INFORMATION
***********************************************************
1
Abaqus 6.14-4 Date 02-Nov-2017 Time 11:45:19
For use at UNIVERSITY OF FLORIDA under license from Dassault Systemes or its subsidiary.
A B A Q U S I N P U T E C H O
*HEADING
Two-dimensional overhead hoist frame
SI units (kg, m, s, N)
1-axis horizontal, 2-axis vertical
LINE 5 *PREPRINT, ECHO=YES, MODEL=YES, HISTORY=YES
**
** Model definition
**
*NODE, NSET=NALL
LINE 10 1, 720., 360., 0.
2, 720., 0., 0.
3, 360., 360., 0.
4, 360., 0., 0.
5, 0., 360., 0.
LINE 15 6, 0., 0., 0.
*ELEMENT, TYPE=T2D2, ELSET=FRAME1
1, 5, 3
*ELEMENT, TYPE=T2D2, ELSET=FRAME2
2, 3, 1
LINE 20 *ELEMENT, TYPE=T2D2, ELSET=FRAME3
3, 6, 4
*ELEMENT, TYPE=T2D2, ELSET=FRAME4
4, 4, 2
*ELEMENT, TYPE=T2D2, ELSET=FRAME5
LINE 25 5, 4, 3
*ELEMENT, TYPE=T2D2, ELSET=FRAME6
6, 2, 1
*ELEMENT, TYPE=T2D2, ELSET=FRAME7
7, 5, 4
LINE 30 *ELEMENT, TYPE=T2D2, ELSET=FRAME8
8, 6, 3
*ELEMENT, TYPE=T2D2, ELSET=FRAME9
9, 3, 2
*ELEMENT, TYPE=T2D2, ELSET=FRAME10
LINE 35 10, 4, 1
*SOLID SECTION, ELSET=FRAME1, MATERIAL=STEEL
** Initial area = 1.0
0.5,
*SOLID SECTION, ELSET=FRAME2, MATERIAL=STEEL
LINE 40 ** Initial area = 1.0
0.5,
*SOLID SECTION, ELSET=FRAME3, MATERIAL=STEEL
** Initial area = 1.0
0.5,
LINE 45 *SOLID SECTION, ELSET=FRAME4, MATERIAL=STEEL
** Initial area = 1.0
0.6,
*SOLID SECTION, ELSET=FRAME5, MATERIAL=STEEL
** Initial area = 1.0
LINE 50 0.7,
*SOLID SECTION, ELSET=FRAME6, MATERIAL=STEEL
** Initial area = 1.0
0.25,
*SOLID SECTION, ELSET=FRAME7, MATERIAL=STEEL
LINE 55 ** Initial area = 1.0
0.25,
*SOLID SECTION, ELSET=FRAME8, MATERIAL=STEEL
** Initial area = 1.0
0.4,
LINE 60 *SOLID SECTION, ELSET=FRAME9, MATERIAL=STEEL
** Initial area = 1.0
0.3,
*SOLID SECTION, ELSET=FRAME10, MATERIAL=STEEL
** Initial area = 1.0
LINE 65 0.7,
*MATERIAL, NAME=STEEL
*ELASTIC
1.E7, 0.3
**
LINE 70 ** History data
**
*STEP, PERTURBATION
P1 & P2
*STATIC
LINE 75 *BOUNDARY
5, 1, 2
6, 1, 2
*CLOAD
2, 2, -66.67E3
LINE 80 4, 2, -66.67E3
*NODE PRINT
U,
RF,
*EL PRINT
LINE 85 S,
**********************************
** OUTPUT FOR ABAQUS QA PURPOSES
**********************************
*EL FILE
LINE 90 S,
*NODE FILE
U, RF
*END STEP
--------------------------------------------------------------------------------
5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80
--------------------------------------------------------------------------------
OPTIONS BEING PROCESSED
***************************
*HEADING
Two-dimensional overhead hoist frame
*NODE, NSET=NALL
*ELEMENT, TYPE=T2D2, ELSET=FRAME1
*ELEMENT, TYPE=T2D2, ELSET=FRAME2
*ELEMENT, TYPE=T2D2, ELSET=FRAME3
*ELEMENT, TYPE=T2D2, ELSET=FRAME4
*ELEMENT, TYPE=T2D2, ELSET=FRAME5
*ELEMENT, TYPE=T2D2, ELSET=FRAME6
*ELEMENT, TYPE=T2D2, ELSET=FRAME7
*ELEMENT, TYPE=T2D2, ELSET=FRAME8
*ELEMENT, TYPE=T2D2, ELSET=FRAME9
*ELEMENT, TYPE=T2D2, ELSET=FRAME10
*MATERIAL, NAME=STEEL
*ELASTIC
*SOLID SECTION, ELSET=FRAME1, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME2, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME3, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME4, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME5, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME6, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME7, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME8, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME9, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME10, MATERIAL=STEEL
*BOUNDARY
*BOUNDARY
*SOLID SECTION, ELSET=FRAME1, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME2, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME3, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME4, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME5, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME6, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME7, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME8, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME9, MATERIAL=STEEL
*SOLID SECTION, ELSET=FRAME10, MATERIAL=STEEL
*STEP, PERTURBATION
*STEP, PERTURBATION
*STEP, PERTURBATION
P1 & P2
*STATIC
*BOUNDARY
*NODE PRINT
*EL PRINT
*EL FILE
*NODE FILE
*END STEP
*STEP, PERTURBATION
*STATIC
*BOUNDARY
*CLOAD
*END STEP
1
Abaqus 6.14-4 Date 02-Nov-2017 Time 11:45:19
For use at UNIVERSITY OF FLORIDA under license from Dassault Systemes or its subsidiary.
Two-dimensional overhead hoist frame
E L E M E N T D E F I N I T I O N S
NUMBER TYPE PROPERTY NODES FORMING ELEMENT
REFERENCE
1 T2D2 1 5 3
2 T2D2 2 3 1
3 T2D2 3 6 4
4 T2D2 4 4 2
5 T2D2 5 4 3
6 T2D2 6 2 1
7 T2D2 7 5 4
8 T2D2 8 6 3
9 T2D2 9 3 2
10 T2D2 10 4 1
S O L I D S E C T I O N (S)
PROPERTY NUMBER 1
MATERIAL NAME STEEL
ATTRIBUTES 0.50000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 2
MATERIAL NAME STEEL
ATTRIBUTES 0.50000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 3
MATERIAL NAME STEEL
ATTRIBUTES 0.50000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 4
MATERIAL NAME STEEL
ATTRIBUTES 0.60000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 5
MATERIAL NAME STEEL
ATTRIBUTES 0.70000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 6
MATERIAL NAME STEEL
ATTRIBUTES 0.25000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 7
MATERIAL NAME STEEL
ATTRIBUTES 0.25000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 8
MATERIAL NAME STEEL
ATTRIBUTES 0.40000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 9
MATERIAL NAME STEEL
ATTRIBUTES 0.30000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
PROPERTY NUMBER 10
MATERIAL NAME STEEL
ATTRIBUTES 0.70000 0.0000 0.0000
HOURGLASS CONTROL STIFFNESS 19231.
(USED WITH LOWER ORDER REDUCED INTEGRATED SOLID ELEMENTS LIKE CPS4R,CPE4RH,C3D8R)
P H Y S I C A L C O N S T A N T S
M A T E R I A L D E S C R I P T I O N
MATERIAL NAME: STEEL
ELASTIC YOUNG'S POISSON'S
MODULUS RATIO
1.00000E+07 0.30000
E L E M E N T S E T S
SET FRAME10
MEMBERS 10
SET FRAME1
MEMBERS 1
SET FRAME2
MEMBERS 2
SET FRAME3
MEMBERS 3
SET FRAME4
MEMBERS 4
SET FRAME5
MEMBERS 5
SET FRAME6
MEMBERS 6
SET FRAME7
MEMBERS 7
SET FRAME8
MEMBERS 8
SET FRAME9
MEMBERS 9
N O D E S E T S
SET NALL
MEMBERS 1 2 3 4 5 6
N O D E D E F I N I T I O N S
NODE COORDINATES SINGLE POINT CONSTRAINTS
NUMBER TYPE PLUS DOF
1 720.00 360.00 0.0000
2 720.00 0.0000 0.0000
3 360.00 360.00 0.0000
4 360.00 0.0000 0.0000
5 0.0000 360.00 0.0000 1 2
6 0.0000 0.0000 0.0000 1 2
1
Abaqus 6.14-4 Date 02-Nov-2017 Time 11:45:19
For use at UNIVERSITY OF FLORIDA under license from Dassault Systemes or its subsidiary.
Two-dimensional overhead hoist frame
S T E P 1 S T A T I C A N A L Y S I S
P1 & P2
FIXED TIME INCREMENTS
TIME INCREMENT IS 2.220E-16
TIME PERIOD IS 2.220E-16
GLOBAL STABILIZATION CONTROL IS NOT USED
THIS IS A LINEAR PERTURBATION STEP.
ALL LOADS ARE DEFINED AS CHANGE IN LOAD TO THE REFERENCE STATE
EXTRAPOLATION WILL NOT BE USED
CHARACTERISTIC ELEMENT LENGTH 420.
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
D A T A B A S E O U T P U T G R O U P 1
THE FOLLOWING FIELD OUTPUT WILL BE WRITTEN EVERY 1 INCREMENT(S)
THE FOLLOWING OUTPUT WILL BE WRITTEN FOR ALL ELEMENTS OF TYPE T2D2. OUTPUT IS AT THE
INTEGRATION POINTS.
S E
THE FOLLOWING OUTPUT WILL BE WRITTEN FOR ALL NODES
U RF CF
END OF DATABASE OUTPUT GROUP 1
D A T A B A S E O U T P U T G R O U P 2
THE FOLLOWING HISTORY OUTPUT WILL BE WRITTEN EVERY 1 INCREMENT(S)
THE FOLLOWING ENERGY OUTPUT QUANTITIES WILL BE WRITTEN FOR THE WHOLE MODEL
ALLKE ALLSE ALLWK ALLPD ALLCD ALLVD ALLKL ALLAE ALLQB
ALLEE ALLIE ETOTAL ALLFD ALLJD ALLSD ALLDMD
ALLCCDW ALLCCE ALLCCEN ALLCCET ALLCCSD ALLCCSDN ALLCCSDT ALLDTI
END OF DATABASE OUTPUT GROUP 2
E L E M E N T P R I N T
THE FOLLOWING TABLE IS PRINTED AT EVERY 1 INCREMENT FOR ALL ELEMENTS OF TYPE T2D2. OUTPUT IS AT
THE INTEGRATION POINTS.
SUMMARIES WILL BE PRINTED WHERE APPLICABLE
TABLE 1S11
E L E M E N T F I L E O U T P U T
THE FOLLOWING TABLE IS OUTPUT AT EVERY 1 INCREMENT FOR ALL ELEMENTS OF TYPE T2D2. OUTPUT IS AT
THE INTEGRATION POINTS.
S
N O D E P R I N T
THE FOLLOWING TABLE IS PRINTED FOR ALL NODES AT EVERY 1 INCREMENT
SUMMARIES WILL BE PRINTED
TABLE 1 U1 U2
THE FOLLOWING TABLE IS PRINTED FOR ALL NODES AT EVERY 1 INCREMENT
SUMMARIES WILL BE PRINTED
TABLE 2 RF1 RF2
N O D E F I L E O U T P U T
THE FOLLOWING TABLE IS OUTPUT FOR ALL NODES AT EVERY 1 INCREMENT
U RF
B O U N D A R Y C O N D I T I O N S
NODE DOF AMP. MAGNITUDE NODE DOF AMP. MAGNITUDE
REF. REF.
5 1 (RAMP) 0.0000 5 2 (RAMP) 0.0000
6 1 (RAMP) 0.0000 6 2 (RAMP) 0.0000
- (RAMP) OR (STEP) - INDICATE USE OF DEFAULT AMPLITUDES ASSOCIATED WITH THE STEP
C O N C E N T R A T E D L O A D S
NODE DOF AMP. AMPLITUDE NODE DOF AMP. AMPLITUDE NODE DOF AMP. AMPLITUDE
REF. REF. REF.
2 2 -66670. 4 2 -66670.
C O N S T R A I N T C H E C K S
PERFORM CONSTRAINT CHECKS: YES
AUTOMATIC MODEL CHANGES: YES
CONSTRAINT CHECKS FREQUENCY: 1
TERMINATE ANALYSIS IF OVERCONSTRAINTS ARE FOUND: NO
P R O B L E M S I Z E
NUMBER OF ELEMENTS IS 10
NUMBER OF NODES IS 6
NUMBER OF NODES DEFINED BY THE USER 6
TOTAL NUMBER OF VARIABLES IN THE MODEL 12
(DEGREES OF FREEDOM PLUS MAX NO. OF ANY LAGRANGE MULTIPLIER
VARIABLES. INCLUDE *PRINT,SOLVE=YES TO GET THE ACTUAL NUMBER.)
END OF USER INPUT PROCESSING
JOB TIME SUMMARY
USER TIME (SEC) = 0.13000
SYSTEM TIME (SEC) = 2.00000E-02
TOTAL CPU TIME (SEC) = 0.15000
WALLCLOCK TIME (SEC) = 0
1
Abaqus 6.14-4 Date 02-Nov-2017 Time 11:45:20
For use at UNIVERSITY OF FLORIDA under license from Dassault Systemes or its subsidiary.
Two-dimensional overhead hoist frame STEP 1 INCREMENT 1
P1 & P2 TIME COMPLETED IN THIS STEP 0.00
S T E P 1 S T A T I C A N A L Y S I S
P1 & P2
FIXED TIME INCREMENTS
TIME INCREMENT IS 2.220E-16
TIME PERIOD IS 2.220E-16
LINEAR EQUATION SOLVER TYPE DIRECT SPARSE
THIS IS A LINEAR PERTURBATION STEP.
ALL LOADS ARE DEFINED AS CHANGE IN LOAD TO THE REFERENCE STATE
M E M O R Y E S T I M A T E
PROCESS FLOATING PT MINIMUM MEMORY MEMORY TO
OPERATIONS REQUIRED MINIMIZE I/O
PER ITERATION (MB) (MB)
1 3.26E+02 13 20
NOTE:
(1) SINCE ABAQUS DOES NOT PRE-ALLOCATE MEMORY AND ONLY ALLOCATES MEMORY AS NEEDED DURING THE ANALYSIS,
THE MEMORY REQUIREMENT PRINTED HERE CAN ONLY BE VIEWED AS A GENERAL GUIDELINE BASED ON THE BEST
KNOWLEDGE AVAILABLE AT THE BEGINNING OF A STEP BEFORE THE SOLUTION PROCESS HAS BEGUN.
(2) THE ESTIMATE IS NORMALLY UPDATED AT THE BEGINNING OF EVERY STEP. IT IS THE MAXIMUM VALUE OF THE
ESTIMATE FROM THE CURRENT STEP TO THE LAST STEP OF THE ANALYSIS, WITH UNSYMMETRIC SOLUTION TAKEN
INTO ACCOUNT IF APPLICABLE.
(3) SINCE THE ESTIMATE IS BASED ON THE ACTIVE DEGREES OF FREEDOM IN THE FIRST ITERATION OF THE
CURRENT STEP, THE MEMORY ESTIMATE MIGHT BE SIGNIFICANTLY DIFFERENT THAN ACTUAL USAGE FOR
PROBLEMS WITH SUBSTANTIAL CHANGES IN ACTIVE DEGREES OF FREEDOM BETWEEN STEPS (OR EVEN WITHIN
THE SAME STEP). EXAMPLES ARE: PROBLEMS WITH SIGNIFICANT CONTACT CHANGES, PROBLEMS WITH MODEL
CHANGE, PROBLEMS WITH BOTH STATIC STEP AND STEADY STATE DYNAMIC PROCEDURES WHERE ACOUSTIC
ELEMENTS WILL ONLY BE ACTIVATED IN THE STEADY STATE DYNAMIC STEPS.
(4) FOR MULTI-PROCESS EXECUTION, THE ESTIMATED VALUE OF FLOATING POINT OPERATIONS FOR EACH PROCESS
IS BASED ON AN INITIAL SCHEDULING OF OPERATIONS AND MIGHT NOT REFLECT THE ACTUAL FLOATING
POINT OPERATIONS COMPLETED ON EACH PROCESS. OPERATIONS ARE DYNAMICALLY BALANCED DURING EXECUTION,
SO THE ACTUAL BALANCE OF OPERATIONS BETWEEN PROCESSES IS EXPECTED TO BE BETTER THAN THE ESTIMATE
PRINTED HERE.
(5) THE UPPER LIMIT OF MEMORY THAT CAN BE ALLOCATED BY ABAQUS WILL IN GENERAL DEPEND ON THE VALUE OF
THE "MEMORY" PARAMETER AND THE AMOUNT OF PHYSICAL MEMORY AVAILABLE ON THE MACHINE. PLEASE SEE
THE "ABAQUS ANALYSIS USER'S MANUAL" FOR MORE DETAILS. THE ACTUAL USAGE OF MEMORY AND OF DISK
SPACE FOR SCRATCH DATA WILL DEPEND ON THIS UPPER LIMIT AS WELL AS THE MEMORY REQUIRED TO MINIMIZE
I/O. IF THE MEMORY UPPER LIMIT IS GREATER THAN THE MEMORY REQUIRED TO MINIMIZE I/O, THEN THE ACTUAL
MEMORY USAGE WILL BE CLOSE TO THE ESTIMATED "MEMORY TO MINIMIZE I/O" VALUE, AND THE SCRATCH DISK
USAGE WILL BE CLOSE-TO-ZERO; OTHERWISE, THE ACTUAL MEMORY USED WILL BE CLOSE TO THE PREVIOUSLY
MENTIONED MEMORY LIMIT, AND THE SCRATCH DISK USAGE WILL BE ROUGHLY PROPORTIONAL TO THE DIFFERENCE
BETWEEN THE ESTIMATED "MEMORY TO MINIMIZE I/O" AND THE MEMORY UPPER LIMIT. HOWEVER ACCURATE
ESTIMATE OF THE SCRATCH DISK SPACE IS NOT POSSIBLE.
(6) USING "*RESTART, WRITE" CAN GENERATE A LARGE AMOUNT OF DATA WRITTEN IN THE WORK DIRECTORY.
INCREMENT 1 SUMMARY
TIME INCREMENT COMPLETED 2.220E-16, FRACTION OF STEP COMPLETED 1.00
STEP TIME COMPLETED 2.220E-16, TOTAL TIME COMPLETED 0.00
E L E M E N T O U T P U T
THE FOLLOWING TABLE IS PRINTED FOR ALL ELEMENTS WITH TYPE T2D2 AT THE INTEGRATION POINTS
ELEMENT PT FOOT- S11
NOTE
1 1 2.8658E+05
2 1 6.4304E+04
3 1 -2.4678E+05
4 1 -5.7530E+04
5 1 6.0145E+04
6 1 1.2861E+05
7 1 3.2086E+05
8 1 -2.7089E+05
9 1 1.6272E+05
10 1 -6.4957E+04
MAXIMUM 3.2086E+05
ELEMENT 7
MINIMUM -2.7089E+05
ELEMENT 8
N O D E O U T P U T
THE FOLLOWING TABLE IS PRINTED FOR ALL NODES
NODE FOOT- U1 U2
NOTE
1 1.2631767E+01 -5.8178898E+01
2 -1.0955216E+01 -6.2808776E+01
3 1.0316828E+01 -2.9820911E+01
4 -8.8841323E+00 -3.1986116E+01
MAXIMUM 12.63 0.000
AT NODE 1 5
MINIMUM -10.96 -62.81
AT NODE 2 2
THE FOLLOWING TABLE IS PRINTED FOR ALL NODES
NODE FOOT- RF1 RF2
NOTE
5 -2.0001000E+05 5.6720726E+04
6 2.0001000E+05 7.6619274E+04
MAXIMUM 2.0001E+05 7.6619E+04
AT NODE 6 6
MINIMUM -2.0001E+05 0.000
AT NODE 5 1
THE ANALYSIS HAS BEEN COMPLETED
ANALYSIS COMPLETE
JOB TIME SUMMARY
USER TIME (SEC) = 6.00000E-02
SYSTEM TIME (SEC) = 1.00000E-02
TOTAL CPU TIME (SEC) = 7.00000E-02
WALLCLOCK TIME (SEC) = 1