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 |