Solid and Shell Elements
Column Number
|
Solid
|
Shell
|
1
|
0
|
0
|
2
|
0
|
0
|
3
|
0
|
0
|
4
|
NORMAL -X
|
NORMAL -X1
|
5
|
NORMAL -Y
|
NORMAL -Y1
|
6
|
NORMAL -Z
|
SHEAR -XY1
|
7
|
SHEAR -XY
|
0
|
8
|
SHEAR -YZ
|
0
|
9
|
SHEAR -ZX
|
0
|
10
|
0
|
0
|
11
|
0
|
VON MISES-1
|
12
|
0
|
FIBER DISTANCE-1
|
13
|
0
|
NORMAL-X2
|
14
|
0
|
NORMAL-Y2
|
15
|
0
|
SHEAR-XY2
|
16
|
0
|
0
|
17
|
0
|
0
|
18
|
0
|
0
|
19
|
0
|
0
|
20
|
0
|
VON MISES-2
|
21
|
0
|
FIBER DISTANCE-2
|
22
|
VON MISES
|
MAX VON MISES-1/2
|
23
|
0
|
0
|
24
|
0
|
0
|
25
|
0
|
0
|
26
|
0
|
0
|
27
|
0
|
0
|
28
|
0
|
0
|
29
|
0
|
0
|
30
|
0
|
0
|
31
|
0
|
0
|
32
|
0
|
0
|
33
|
0
|
MEMBRANE FX
|
34
|
0
|
MEMBRANE FY
|
35
|
0
|
MEMBRANE FXY
|
36
|
0
|
MOMENT MX
|
37
|
0
|
MOMENT MY
|
38
|
0
|
MOMENT MXY
|
39
|
0
|
TRANSV. SHEAR QX
|
40
|
0
|
TRANSV. SHEAR QY
|
Note: Complex data is stored as columns 1-40 are real/magnitude and columns 41-80 are imaginary/phase. When
STRESS(CORNER) is specified in the Case Control Section of the model, columns 1-80 for solid and shell elements are repeated for each element node. The corresponding column number is equal to:
COLUMN NUMBER + (80 x NODE NUMBER).
Line Elements (Bar/Beam, Rod, Spring)
Column Number
|
Bar/Beam
|
Rod
|
Spring
|
1
|
0
|
0
|
0
|
2
|
0
|
0
|
0
|
3
|
0
|
0
|
0
|
4
|
SA-AXIAL
|
S-AXIAL
|
STRESS
|
5
|
SA-C
|
S-TORSIONAL
|
0
|
6
|
SA-D
|
0
|
0
|
7
|
SA-E
|
0
|
0
|
8
|
SA-F
|
0
|
0
|
9
|
SB-AXIAL
|
0
|
0
|
10
|
SB-C
|
0
|
0
|
11
|
SB-D
|
0
|
0
|
12
|
SB-E
|
0
|
0
|
13
|
SB-F
|
0
|
0
|
14
|
SA-MIN
|
0
|
0
|
15
|
SB-MIN
|
0
|
0
|
16
|
SA-MAX
|
0
|
0
|
17
|
SB-MAX
|
0
|
0
|
18
|
S-MAX
|
0
|
0
|
19
|
S-MIN
|
0
|
0
|
20
|
0
|
0
|
0
|
21
|
0
|
0
|
0
|
22
|
0
|
0
|
0
|
23
|
LOCATION A
|
0
|
0
|
24
|
LOCATION B
|
0
|
0
|
25
|
LOCATION S-MAX
|
0
|
0
|
26
|
LOCATION S-MIN
|
0
|
0
|
27
|
0
|
0
|
0
|
28
|
0
|
0
|
0
|
29
|
FORCE A-X
|
FORCE A-X
|
FORCE
|
30
|
FORCE A-Y PLANE 1
|
0
|
0
|
31
|
FORCE A-Z PLANE 2
|
0
|
0
|
32
|
MOMENT A-X
|
MOMENT A-X
|
0
|
33
|
MOMENT A-Y PLANE 2
|
0
|
0
|
34
|
MOMENT A-Z PLANE 1
|
0
|
0
|
35
|
FORCE B-X
|
FORCE B-X
|
0
|
36
|
FORCE B-Y
|
0
|
0
|
37
|
FORCE B-Z
|
0
|
0
|
38
|
MOMENT B-X
|
MOMENT B-X
|
0
|
39
|
MOMENT B-Y PLANE 2
|
0
|
0
|
40
|
MOMENT B-Z PLANE 1
|
0
|
0
|
Note: Complex data is stored as columns 1-40 are real/magnitude and columns 41-80 are imaginary/phase.
Line Elements (Weld, Bush)
Column Number
|
Weld
|
Bush
|
1
|
0
|
0
|
2
|
0
|
0
|
3
|
0
|
0
|
4
|
SA-LONGITUDINAL
|
S-TX
|
5
|
SA-TORSIONAL
|
S-TY
|
6
|
SA-SHEAR
|
S-TZ
|
7
|
0
|
S-RX
|
8
|
0
|
S-RY
|
9
|
SB-LONGITUDINAL
|
S-RZ
|
10
|
SB-TORSIONAL
|
S-T MAX
|
11
|
SB-SHEAR
|
S-R MAX
|
12
|
0
|
0
|
13
|
0
|
0
|
14
|
S-MAX LONGITUDINAL
|
0
|
15
|
S-MAX TORSIONAL
|
0
|
16
|
S-MAX SHEAR
|
0
|
17
|
0
|
0
|
18
|
0
|
0
|
19
|
0
|
0
|
20
|
0
|
0
|
21
|
0
|
0
|
22
|
0
|
0
|
23
|
LOCATION A
|
0
|
24
|
LOCATION B
|
0
|
25
|
0
|
0
|
26
|
0
|
0
|
27
|
0
|
0
|
28
|
0
|
0
|
29
|
FORCE A-X
|
VISC DAMP FORCE-X
|
30
|
FORCE A-Y PLANE 1
|
VISC DAMP FORCE-Y
|
31
|
FORCE A-Z PLANE 2
|
VISC DAMP FORCE-Z
|
32
|
MOMENT A-X
|
VISC DAMP MOMENT-X
|
33
|
MOMENT A-Y PLANE 2
|
VISC DAMP MOMENT-Y
|
34
|
MOMENT A-Z PLANE 1
|
VISC DAMP MOMENT-Z
|
35
|
FORCE B-X
|
FORCE-X
|
36
|
FORCE B-Y
|
FORCE-Y
|
37
|
FORCE B-Z
|
FORCE-Z
|
38
|
MOMENT B-X
|
MOMENT-X
|
39
|
MOMENT B-Y PLANE 2
|
MOMENT-Y
|
40
|
MOMENT B-Z PLANE 1
|
MOMENT-Z
|