| Project: |  | |
| Project no: | ||
| Author: |
Project data
| Project name | |
| Project number | |
| Author | |
| Description | |
| Date | 13/06/2024 |
| Design code | AISC |
Geometry
Analyzed members
AM1
| Property | Value |
|---|---|
| Name | AM1 |
| Members | M2 |
| Cross-section | W10X60 |
| Length | 24.00 ft |
| ey | 0.00 in |
| ez | 0.00 in |
| Begin | (0.00; 0.00; 0.00) ft |
| End | (24.00; 0.00; 0.00) ft |
Related members
RM2
| Property | Value |
|---|---|
| Name | RM2 |
| Members | M4 |
| Cross-section | W10X60 |
| Length | 24.00 ft |
| ey | 0.00 in |
| ez | 0.00 in |
| Begin | (0.00; 0.00; -12.00) ft |
| End | (0.00; 0.00; 12.00) ft |
| Support Begin | ■ X | ■ Y | ■ Z | □ Rx | □ Ry | □ Rz |
| Support End | ■ X | ■ Y | ■ Z | □ Rx | □ Ry | □ Rz |
RM4
| Property | Value |
|---|---|
| Name | RM4 |
| Members | M6 |
| Cross-section | W10X60 |
| Length | 24.00 ft |
| ey | 0.00 in |
| ez | 0.00 in |
| Begin | (24.00; 0.00; -12.00) ft |
| End | (24.00; 0.00; 12.00) ft |
| Support Begin | ■ X | ■ Y | ■ Z | □ Rx | □ Ry | □ Rz |
| Support End | ■ X | ■ Y | ■ Z | □ Rx | □ Ry | □ Rz |
Cross-section
W10X60, Material: A36
Loading
LE1 – Type ULS
Line load
Member |
Begin [ft] |
End [ft] |
X [kip/ft] |
Y [kip/ft] |
Z [kip/ft] |
Location |
Width [in] |
Ey [in] |
|---|---|---|---|---|---|---|---|---|
| AM1 | 0.00 | 24.00 | 0.00 | 0.00 | -1.50 | Top | 4.00 | 0.00 |
Point load
Member |
N [kip] |
Vy [kip] |
Vz [kip] |
Mx [kip] |
My [kip] |
Mz [kip] |
|---|---|---|---|---|---|---|
| RM2 / Begin | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| RM2 / End | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| RM4 / Begin | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| RM4 / End | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
Results
Materially non-linear analysis (MNA)
Summary
Load |
Applied loads [%] |
|---|---|
| LE1 | 100.0 |
Eq. stress ,LC1
Plastic strain ,LC1
Design data
Material |
fy [ksi] |
εlim [%] |
|---|---|---|
| A36 | 36.0 | 5.0 |
Linear buckling analysis (LBA)
Normalized deflection, LE1, Buckling shape 1
Geometrically and materially non-linear analysis with imperfections (GMNIA)
Summary
Load |
Applied loads [%] |
|---|---|
| LE1 | 100.0 |
Imperfections
Loads |
1 |
2 |
3 |
4 |
5 |
6 |
|
|---|---|---|---|---|---|---|---|
| LE1 | Buckling factor [-] | 3.86 | 14.32 | 22.98 | 22.98 | 24.57 | 24.57 |
| Amplitude [in] | 0.50 | 0.50 | 0.00 | 0.00 | 0.00 | 0.00 |
Eq. stress ,LC1
Plastic strain ,LC1
Design data
Material |
fy [ksi] |
εlim [%] |
|---|---|---|
| A36 | 36.0 | 5.0 |
Symbol explanation
Symbol |
Explanation |
|---|---|
| fy | Yield strength |
| εlim | Limit of plastic strain used in 2D plate element check |
Code settings
| Stop at limit strain | No | |
| Pretension force factor k | 0.70 | - |
| Friction coefficient in slip-resistance | 0.30 | - |
| Anchor length for stiffness calculation [d] | 8 | |
| Limit plastic strain | 500.0 | 1e-4 |
| Division of surface of the biggest circular hollow member | 64 | |
| Division of arc of rectangular hollow member | 3 | |
| Number of elements on biggest member web or flange | 8 | |
| Number of elements on biggest web of RHS member | 16 | |
| Number of elements on individual plates | 20 | |
| Number of analysis iterations | 25 | |
| Divergent iterations count | 6 | |
| Minimal size of element | 0.39 | in |
| Maximal size of element | 1.97 | in |
| Number of buckling modes | 6 |
Software info
| Application | IDEA StatiCa Member |
| Version | 24.0.2.1309 |
| Developed by | IDEA StatiCa |