📄 sample4a.out
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INPUT FILE: SAMPLE4A.IN OUTPUT FILE: SAMPLE4A.OUT
PPPPP CCCCC SSSSS AAAA PPPPP 4 4
P P C S A A P P 4 4
PPPPP C ** SSSSS AAAAAA PPPPP 4444444
P C S A A P 4
P CCCC SSSSS A A P 4
By
Bruce F. Maison
August 1994
Based On SAP-4 Developed By
K.J. Bathe, E.L. Wilson, F.E. Peterson
University of California, Berkeley
** SAMPLE ANALYSIS 4A ** SRSS RESPONSE SPECTRUM ANALYSIS
C O N T R O L I N F O R M A T I O N
NUMBER OF NODAL POINTS = 14
NUMBER OF ELEMENT TYPES = 1
NUMBER OF LOAD CASES = 1
NUMBER OF FREQUENCIES = 5
ANALYSIS CODE (NDYN) = 3
EQ.0, STATIC
EQ.1, MODAL EXTRACTION
EQ.2, FORCED RESPONSE
EQ.3, RESPONSE SPECTRUM
EQ.4, DIRECT INTEGRATION
SOLUTION MODE (MODEX) = 0
EQ.0, EXECUTION
EQ.1, DATA CHECK
NUMBER OF SUBSPACE
ITERATION VECTORS (NAD) = 0
EQUATIONS PER BLOCK = 0
TAPE10 SAVE FLAG (N10SV) = 0
STORAGE CAPACITY (MTOT) = 500000
NODAL POINT INPUT DATA
NODE BOUNDARY CONDITION CODES NODAL POINT COORDINATES
NUMBER X Y Z XX YY ZZ X Y Z T
1 1 1 1 1 1 1 0.000 0.000 0.000 0 0.000
2 0 0 0 0 0 0 100.000 0.000 0.000 0 0.000
3 0 0 0 0 0 0 200.000 0.000 0.000 0 0.000
4 0 0 0 0 0 0 225.456 -10.544 0.000 0 0.000
5 0 0 0 0 0 0 300.456 -85.544 0.000 0 0.000
6 0 0 0 0 0 0 325.912 -96.088 0.000 0 0.000
7 0 1 0 0 0 0 375.912 -96.088 0.000 0 0.000
8 0 0 0 0 0 0 425.912 -96.088 0.000 0 0.000
9 0 0 0 0 0 0 425.912 -96.088 70.000 0 0.000
10 0 1 0 0 0 0 475.912 -96.088 0.000 0 0.000
11 0 0 0 0 0 0 407.912 -96.088 88.000 0 0.000
12 0 0 0 0 0 0 557.912 -96.088 0.000 0 0.000
13 0 0 0 0 0 0 337.912 -96.088 88.000 0 0.000
14 0 1 0 0 0 0 267.912 -96.088 88.000 0 0.000
GENERATED NODAL DATA
NODE BOUNDARY CONDITION CODES NODAL POINT COORDINATES
NUMBER X Y Z XX YY ZZ X Y Z T
1 1 1 1 1 1 1 0.000 0.000 0.000 0.000
2 0 0 0 0 0 0 100.000 0.000 0.000 0.000
3 0 0 0 0 0 0 200.000 0.000 0.000 0.000
4 0 0 0 0 0 0 225.456 -10.544 0.000 0.000
5 0 0 0 0 0 0 300.456 -85.544 0.000 0.000
6 0 0 0 0 0 0 325.912 -96.088 0.000 0.000
7 0 1 0 0 0 0 375.912 -96.088 0.000 0.000
8 0 0 0 0 0 0 425.912 -96.088 0.000 0.000
9 0 0 0 0 0 0 425.912 -96.088 70.000 0.000
10 0 1 0 0 0 0 475.912 -96.088 0.000 0.000
11 0 0 0 0 0 0 407.912 -96.088 88.000 0.000
12 0 0 0 0 0 0 557.912 -96.088 0.000 0.000
13 0 0 0 0 0 0 337.912 -96.088 88.000 0.000
14 0 1 0 0 0 0 267.912 -96.088 88.000 0.000
EQUATION NUMBERS
N X Y Z XX YY ZZ
1 0 0 0 0 0 0
2 1 2 3 4 5 6
3 7 8 9 10 11 12
4 13 14 15 16 17 18
5 19 20 21 22 23 24
6 25 26 27 28 29 30
7 31 0 32 33 34 35
8 36 37 38 39 40 41
9 42 43 44 45 46 47
10 48 0 49 50 51 52
11 53 54 55 56 57 58
12 59 60 61 62 63 64
13 65 66 67 68 69 70
14 71 0 72 73 74 75
P I P E E L E M E N T I N P U T D A T A
C O N T R O L I N F O R M A T I O N
NUMBER OF PIPE ELEMENTS = 13
NUMBER OF MATERIAL SETS = 2
MAXIMUM NUMBER OF MATERIAL
TEMPERATURE INPUT POINTS = 1
NUMBER OF SECTION PROPERTY SETS = 2
NUMBER OF BRANCH POINT NODES = 0
MAXIMUM NUMBER OF TANGENTS
COMMON TO A BRANCH POINT = 4
FLAG FOR NEGLECTING AXIAL
DEFORMATIONS IN BEND ELEMENTS = 0
(EQ.1, NEGLECT)
M A T E R I A L P R O P E R T Y T A B L E S
MATERIAL NUMBER = ( 1)
NUMBER OF
TEMPERATURE POINTS = ( 1)
IDENTIFICATION = ( 75 F CARBON STEEL )
POINT YOUNG*S POISSON*S THERMAL
NUMBER TEMPERATURE MODULUS RATIO EXPANSION
1 0.00 29000000.0 0.300 0.000E+00
MATERIAL NUMBER = ( 2)
NUMBER OF
TEMPERATURE POINTS = ( 1)
IDENTIFICATION = (200 F CARBON STEEL )
POINT YOUNG*S POISSON*S THERMAL
NUMBER TEMPERATURE MODULUS RATIO EXPANSION
1 0.00 29000000.0 0.300 0.000E+00
S E C T I O N P R O P E R T Y T A B L E
SECTION OUTSIDE WALL SHAPE FACTOR WEIGHT/ MASS/
NUMBER DIAMETER THICKNESS FOR SHEAR UNIT LENGTH UNIT LENGTH D E S C R I P T I O N
1 24.000 0.6870 0.0000 0.2875E+02 0.7440E-01 24 INCH- SCHD.40
2 12.750 0.4060 0.0000 0.8500E+01 0.2200E-01 12 INCH- SCHD.40
E L E M E N T L O A D C A S E M U L T I P L I E R S
CASE A CASE B CASE C CASE D
X-DIRECTION GRAVITY 0.000 0.000 0.000 0.000
Y-DIRECTION GRAVITY 0.000 0.000 0.000 0.000
Z-DIRECTION GRAVITY 0.000 0.000 0.000 0.000
THERMAL DISTORTION 0.000 0.000 0.000 0.000
PRESSURE DISTORTION 0.000 0.000 0.000 0.000
P I P E E L E M E N T I N P U T D A T A
ELEMENT ELEMENT NODE NODE MATL. SECTION REFERENCE INTERNAL D I R E C T I O N C O S I N E S NODE INPUT
NUMBER TYPE -I -J NUMBER NUMBER TEMPERATURE PRESSURE A(YX) A(YY) A(YZ) INCREMENT TAG
(BEND (THIRD (X3- (Y3- (Z3- (WALL
RADIUS) POINT) ORDINATE) ORDINATE) ORDINATE) FRACTION)
1 TANGENT 1 2 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
2 TANGENT 2 3 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
3 TANGENT 4 5 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
4 TANGENT 6 7 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
5 TANGENT 7 8 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
6 TANGENT 8 10 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
7 TANGENT 10 12 1 1 0.00 0.00 0.0000 0.0000 0.0000 1 II
8 TANGENT 8 9 1 2 0.00 0.00 0.0000 0.0000 0.0000 1 II
9 TANGENT 11 13 2 2 0.00 0.00 0.0000 0.0000 0.0000 1 II
10 TANGENT 13 14 2 2 0.00 0.00 0.0000 0.0000 0.0000 1 II
11 BEND 3 4 1 1 0.00 0.00 IC
( 36.000) (TI) ( 214.912)( 0.000)( 0.000) ( 0.1000)
12 BEND 5 6 1 1 0.00 0.00 IC
( 36.000) (TI) ( 311.000)( -96.088)( 0.000) ( 0.1000)
13 BEND 9 11 2 2 0.00 0.00 IC
( 18.000) (TI) ( 425.912)( -96.088)( 88.000) ( 0.1000)
E Q U A T I O N P A R A M E T E R S
TOTAL NUMBER OF EQUATIONS = 75
BANDWIDTH = 18
NUMBER OF EQUATIONS IN A BLOCK = 75
NUMBER OF BLOCKS = 1
N O D A L L O A D S (S T A T I C) O R M A S S E S (D Y N A M I C)
NODE LOAD X-AXIS Y-AXIS Z-AXIS X-AXIS Y-AXIS Z-AXIS
NUMBER CASE FORCE FORCE FORCE MOMENT MOMENT MOMENT
2 0 0.18116E+02 0.18116E+02 0.18116E+02 0.00000E+00 0.00000E+00 0.00000E+00
STRUCTURE ELEMENT LOAD MULTIPLIERS
LOAD CASE A B C D
1 0.000 0.000 0.000 0.000
E I G E N V A L U E A N A L Y S I S
DETERMINANT SEARCH SOLUTION IS CARRIED OUT
CONTROL INFORMATION
FLAG FOR ADDITIONAL PRINTING = 1
EQ.0, SUPPRESS
EQ.1, PRINT
STURM SEQUENCE CHECK FLAG (*) = 0
EQ.0, PERFORM CHECK
EQ.1, PASS
MAXIMUM ITERATION CYCLES (*) = 16
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