***** ANSYS SOLVE COMMAND ***** S O L U T I O N O P T I O N S PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D DEGREES OF FREEDOM. . . . . . UX UY UZ ROTX ROTY ROTZ ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE) *** NOTE *** CP= 1.001 TIME= 14:44:15 Present time 0 is less than or equal to the previous time. Time will default to 1. L O A D S T E P O P T I O N S LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1 TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000 NUMBER OF SUBSTEPS. . . . . . . . . . . . . . . 1 STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO PRINT OUTPUT CONTROLS ITEM FREQUENCY COMPONENT BASI ALL NLOA ALL DATABASE OUTPUT CONTROLS. . . . . . . . . . . .ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= file.mntr Estimated number of active DOF= 12. Maximum wavefront= 28. Range of element maximum matrix coefficients in global coordinates Maximum= 1423534.17 at element 2. Minimum= 741424.047 at element 1. *** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 2 PIPE16 0.000 0.000000 Time at end of element matrix formulation CP= 1.2918576. Time at end of matrix assembly CP= 1.2918576. SPARSE MATRIX DIRECT SOLVER. Number of equations = 12, Maximum wavefront = 28 Memory available for solver = 0.76 MB Memory required for in-core = 0.00 MB Optimal memory required for out-of-core = 0.00 MB Least memory required for out-of-core = 0.00 MB 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ***** ANSYS/University low option 00228540 VERSION=INTEL NT 14:44:17 FEB 23, 2004 CP= 1.793 Your name, ME 421, and date here, torq1.a ********************************************************* * * * ANSYS VERSION FOR UNIVERSITY TEACHING PURPOSES ONLY * * * ********************************************************* ***** DEGREE OF FREEDOM SOLUTION ***** TIME = 1.0000 LOAD STEP= 1 SUBSTEP = 1 CUM. ITER.= 1 NOTE - ALL VECTOR DOFS ARE IN NODAL COORDINATE SYSTEMS. NODE UX UY UZ ROTX ROTY ROTZ 1 0.00000 0.00000 0.00000 0.327191E-01 0.00000 0.00000 2 0.00000 0.00000 0.00000 -0.388035E-01 0.00000 0.00000 3 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 MAXIMUMS NODE 0 0 0 2 0 0 VALUE 0.00000 0.00000 0.00000 -0.388035E-01 0.00000 0.00000 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ***** ANSYS/University low option 00228540 VERSION=INTEL NT 14:44:17 FEB 23, 2004 CP= 1.793 Your name, ME 421, and date here, torq1.a ********************************************************* * * * ANSYS VERSION FOR UNIVERSITY TEACHING PURPOSES ONLY * * * ********************************************************* ***** ELEMENT SOLUTION ***** TIME = 1.0000 LOAD STEP= 1 SUBSTEP = 1 CUM. ITER.= 1 EL= 1 NODES= 1 2 MAT= 1 STR PIPE-PIPE16 SFACTI= 1.0000 SFACTJ= 1.0000 S1MX= 10430. S3MN= -10430. SINTMX= 20861. SEQVMX= 18066. ANGLE 0 45 90 135 180 225 270 315 END I SAXL 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SRAD 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SH 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SXH 10430. 10430. 10430. 10430. 10430. 10430. 10430. 10430. S1 10430. 10430. 10430. 10430. 10430. 10430. 10430. 10430. S3 -10430. -10430. -10430. -10430. -10430. -10430. -10430. -10430. SINT 20861. 20861. 20861. 20861. 20861. 20861. 20861. 20861. SEQV 18066. 18066. 18066. 18066. 18066. 18066. 18066. 18066. EPELAXL 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELRAD 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELH 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELXH 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 END J SAXL 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SRAD 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SH 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SXH 10430. 10430. 10430. 10430. 10430. 10430. 10430. 10430. S1 10430. 10430. 10430. 10430. 10430. 10430. 10430. 10430. S3 -10430. -10430. -10430. -10430. -10430. -10430. -10430. -10430. SINT 20861. 20861. 20861. 20861. 20861. 20861. 20861. 20861. SEQV 18066. 18066. 18066. 18066. 18066. 18066. 18066. 18066. EPELAXL 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELRAD 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELH 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELXH 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 0.0009313 STATIC LOAD ON NODE 1 0.00000 0.00000 0.00000 -4000.00 0.00000 0.00000 STATIC LOAD ON NODE 2 0.00000 0.00000 0.00000 4000.00 0.00000 0.00000 EL= 2 NODES= 2 3 MAT= 1 STR PIPE-PIPE16 SFACTI= 1.0000 SFACTJ= 1.0000 S1MX= 9054.1 S3MN= -9054.1 SINTMX= 18108. SEQVMX= 15682. ANGLE 0 45 90 135 180 225 270 315 END I SAXL 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SRAD 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SH 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SXH -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 S1 9054.1 9054.1 9054.1 9054.1 9054.1 9054.1 9054.1 9054.1 S3 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 SINT 18108. 18108. 18108. 18108. 18108. 18108. 18108. 18108. SEQV 15682. 15682. 15682. 15682. 15682. 15682. 15682. 15682. EPELAXL 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELRAD 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELH 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELXH -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 END J SAXL 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SRAD 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SH 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 SXH -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 S1 9054.1 9054.1 9054.1 9054.1 9054.1 9054.1 9054.1 9054.1 S3 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 -9054.1 SINT 18108. 18108. 18108. 18108. 18108. 18108. 18108. 18108. SEQV 15682. 15682. 15682. 15682. 15682. 15682. 15682. 15682. EPELAXL 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELRAD 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELH 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 0.0000000 EPELXH -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 -0.0008084 STATIC LOAD ON NODE 2 0.00000 0.00000 0.00000 6000.00 0.00000 0.00000 STATIC LOAD ON NODE 3 0.00000 0.00000 0.00000 -6000.00 0.00000 0.00000 *** ELEMENT RESULT CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 2 PIPE16 0.000 0.000000 *** NODAL LOAD CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 2 PIPE16 0.000 0.000000 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ***** ANSYS/University low option 00228540 VERSION=INTEL NT 14:44:17 FEB 23, 2004 CP= 1.823 Your name, ME 421, and date here, torq1.a ********************************************************* * * * ANSYS VERSION FOR UNIVERSITY TEACHING PURPOSES ONLY * * * ********************************************************* ***** REACTION SOLUTION ***** TIME = 1.0000 LOAD STEP= 1 SUBSTEP = 1 CUM. ITER.= 1 NOTE - ALL VECTOR DOFS ARE IN NODAL COORDINATE SYSTEMS. NODE FX FY FZ MX MY MZ 3 0.00000 0.00000 0.00000 6000.00 0.00000 0.00000 TOTAL 0.00000 0.00000 0.00000 6000.00 0.00000 0.00000 *** NOTE *** CP= 1.823 TIME= 14:44:17 Totals may not be correct if any reaction nodes are in a rotated nodal coordinate system. *** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1 *** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX *** PROBLEM STATISTICS ACTUAL NO. OF ACTIVE DEGREES OF FREEDOM = 12 R.M.S. WAVEFRONT SIZE = 0.0 *** ANSYS BINARY FILE STATISTICS BUFFER SIZE USED= 16384 0.063 MB WRITTEN ON ELEMENT MATRIX FILE: file.emat 0.063 MB WRITTEN ON ELEMENT SAVED DATA FILE: file.esav 0.063 MB WRITTEN ON ASSEMBLED MATRIX FILE: file.full 0.063 MB WRITTEN ON RESULTS FILE: file.rst ALL BOUNDARY CONDITION DISPLAY KEYS SET TO 1 FINISH SOLUTION PROCESSING ***** ROUTINE COMPLETED ***** CP = 1.883 ***** ANSYS RESULTS INTERPRETATION (POST1) ***** ENTER /SHOW,DEVICE-NAME TO ENABLE GRAPHIC DISPLAY ENTER FINISH TO LEAVE POST1 *** NOTE *** CP= 1.883 TIME= 14:44:17 Reading results into the database (SET command) will update the current displacement and force boundary conditions in the database with the values from the results file for that load set. Note that any subsequent solutions will use these values unless action is taken to either SAVE the current values or not overwrite them (/EXIT,NOSAVE). STORE STR FROM ITEM=LS COMP= 1 FOR ALL SELECTED ELEMENTS /OUTPUT FILE= D:\Ansys\Rotate.txt