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A 4 m UC 203 x 203 x 46 cantilever column in 3D, fixed at its base, with 300 kN down on top and horizontal loads of 10 kN along X (strong-axis bending) and 5 kN along Y (weak-axis bending). The normal stress is sigma = N/A - Mz y/Iz - My z/Iy: uniform under the axial load alone, a tilted plane once it bends, and worst at a corner when it bends both ways.
| member | N extreme (kN) | |Vy| (kN) | |Vz| (kN) | |My| (kN·m) | |Mz| (kN·m) | |T| (kN·m) | |
|---|---|---|---|---|---|---|---|
| col | -300.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | C |
| node | ux (mm) | uy (mm) | uz (mm) | rx (mrad) | ry (mrad) | rz (mrad) |
|---|---|---|---|---|---|---|
| base | 0.00 | 0.00 | 0.00 | 0.000 | 0.000 | 0.000 |
| top | 0.00 | 0.00 | -0.97 | 0.000 | 0.000 | 0.000 |
| node | Rx (kN) | Ry (kN) | Rz (kN) | Mx (kN·m) | My (kN·m) | Mz (kN·m) |
|---|---|---|---|---|---|---|
| base | 0.00 | 0.00 | 300.00 | 0.00 | 0.00 | 0.00 |
✔ Global equilibrium satisfied · force error 0.0e+0% · moment error 0.0e+0%
Engine 0.1.0+3321a326faba · 16:55:45 UTC · educational tool - verify results independently