📄 sample6.out
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INPUT FILE: SAMPLE6.IN OUTPUT FILE: SAMPLE6.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 6 ** MODE SUPERPOSITION TIME HISTORY ANALYSIS
C O N T R O L I N F O R M A T I O N
NUMBER OF NODAL POINTS = 32
NUMBER OF ELEMENT TYPES = 1
NUMBER OF LOAD CASES = 0
NUMBER OF FREQUENCIES = 20
ANALYSIS CODE (NDYN) = 2
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 0 0 1 1 1 0.000 2.850 0.000 0 0.000
29 1 0 0 1 1 1 0.000 2.850 8.400 2 0.000
31 1 0 1 1 1 1 0.000 2.850 9.000 0 0.000
2 1 1 0 1 1 1 0.000 3.150 0.000 0 0.000
4 1 0 0 1 1 1 0.000 3.150 0.600 0 0.000
30 1 0 0 1 1 1 0.000 3.150 8.400 2 0.000
32 1 0 1 1 1 1 0.000 3.150 9.000 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 0 0 1 1 1 0.000 2.850 0.000 0.000
2 1 1 0 1 1 1 0.000 3.150 0.000 0.000
3 1 0 0 1 1 1 0.000 2.850 0.600 0.000
4 1 0 0 1 1 1 0.000 3.150 0.600 0.000
5 1 0 0 1 1 1 0.000 2.850 1.200 0.000
6 1 0 0 1 1 1 0.000 3.150 1.200 0.000
7 1 0 0 1 1 1 0.000 2.850 1.800 0.000
8 1 0 0 1 1 1 0.000 3.150 1.800 0.000
9 1 0 0 1 1 1 0.000 2.850 2.400 0.000
10 1 0 0 1 1 1 0.000 3.150 2.400 0.000
11 1 0 0 1 1 1 0.000 2.850 3.000 0.000
12 1 0 0 1 1 1 0.000 3.150 3.000 0.000
13 1 0 0 1 1 1 0.000 2.850 3.600 0.000
14 1 0 0 1 1 1 0.000 3.150 3.600 0.000
15 1 0 0 1 1 1 0.000 2.850 4.200 0.000
16 1 0 0 1 1 1 0.000 3.150 4.200 0.000
17 1 0 0 1 1 1 0.000 2.850 4.800 0.000
18 1 0 0 1 1 1 0.000 3.150 4.800 0.000
19 1 0 0 1 1 1 0.000 2.850 5.400 0.000
20 1 0 0 1 1 1 0.000 3.150 5.400 0.000
21 1 0 0 1 1 1 0.000 2.850 6.000 0.000
22 1 0 0 1 1 1 0.000 3.150 6.000 0.000
23 1 0 0 1 1 1 0.000 2.850 6.600 0.000
24 1 0 0 1 1 1 0.000 3.150 6.600 0.000
25 1 0 0 1 1 1 0.000 2.850 7.200 0.000
26 1 0 0 1 1 1 0.000 3.150 7.200 0.000
27 1 0 0 1 1 1 0.000 2.850 7.800 0.000
28 1 0 0 1 1 1 0.000 3.150 7.800 0.000
29 1 0 0 1 1 1 0.000 2.850 8.400 0.000
30 1 0 0 1 1 1 0.000 3.150 8.400 0.000
31 1 0 1 1 1 1 0.000 2.850 9.000 0.000
32 1 0 1 1 1 1 0.000 3.150 9.000 0.000
EQUATION NUMBERS
N X Y Z XX YY ZZ
1 0 1 2 0 0 0
2 0 0 3 0 0 0
3 0 4 5 0 0 0
4 0 6 7 0 0 0
5 0 8 9 0 0 0
6 0 10 11 0 0 0
7 0 12 13 0 0 0
8 0 14 15 0 0 0
9 0 16 17 0 0 0
10 0 18 19 0 0 0
11 0 20 21 0 0 0
12 0 22 23 0 0 0
13 0 24 25 0 0 0
14 0 26 27 0 0 0
15 0 28 29 0 0 0
16 0 30 31 0 0 0
17 0 32 33 0 0 0
18 0 34 35 0 0 0
19 0 36 37 0 0 0
20 0 38 39 0 0 0
21 0 40 41 0 0 0
22 0 42 43 0 0 0
23 0 44 45 0 0 0
24 0 46 47 0 0 0
25 0 48 49 0 0 0
26 0 50 51 0 0 0
27 0 52 53 0 0 0
28 0 54 55 0 0 0
29 0 56 57 0 0 0
30 0 58 59 0 0 0
31 0 60 0 0 0 0
32 0 61 0 0 0 0
AXISYMMETRIC ANALYSIS
NUMBER OF ELEMENTS = 15
NUMBER OF MATERIALS = 1
MAXIMUM TEMPERATURES
PER MATERIAL = 1
ANALYSIS CODE = 0
CODE FOR INCLUSION
OF BENDING MODES = 0
EQ.0, INCLUDE
GT.0, SUPPRESS
MATERIAL I.D. NUMBER = 1
NUMBER OF TEMPERATURES = 1
WEIGHT DENSITY = 0.0000E+00
MASS DENSITY = 0.3663E-01
BETA ANGLE = 0.000
TEMPERATURE E(N) E(S) E(T) NU(NS) NU(NT) NU(ST) G(NS) ALPHA(N) ALPHA(S) ALPHA(T)
0.00 0.3000E+08 0.3000E+08 0.3000E+08 0.3000 0.3000 0.3000 0.1154E+08 0.0000E+00 0.0000E+00 0.0000E+00
ELEMENT LOAD MULTIPLIERS
LOAD CASE TEMPERATURE PRESSURE X-GRAVITY Y-GRAVITY Z-GRAVITY
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