Description
Prove that coupling of different dimensional elements doesn't affect the results. A cantilever with a rectangular cross-section is fixed at one end and loaded at the other with forces Fx and Fz. Neglecting its self-weight and assuming only small deformations, determine cantilever's maximum axial deflection ux, transversal deflection uz, and total deflection u.
| Material | Linear Elastic | Modulus of Elasticity | E | 200000.000 | MPa |
| Poisson's Ratio | ν | 0.000 | - | ||
| Geometry | Cantilever | Length | L | 1.000 | m |
| Width | b | 100.000 | mm | ||
| Height | h | 10.000 | mm | ||
| Load | Axial Force | Fx | 1000.000 | kN | |
| Transversal Force | Fz | 0.100 | kN | ||
Analytical Solution
Deflection of the cantilever with a rectangular cross-section in the axial (X) direction can be calculated according to the following formula:
Deflection in the transversal direction (Z), including shear effect, can be calculated according to the following formula:
Parameter β is for the rectangular cross-section equal to 1.2. Finally, the total deflection of the cantilever can be calculated.
RFEM Settings
- Modeled in version RFEM 5.26 and RFEM 6.06
- The element size is lFE= 0.010 m
- Geometrically linear analysis is considered
- The Mindlin plate theory is used
- Isotropic linear elastic material model is used
- Shear stiffness of members is activated
Results
| Quantity | Analytical Solution | RFEM 6 (Plate-Member) | RFEM 6 (Solid-Member) | RFEM 6 (Solid-Plate) | |||
| [mm] | [mm] | Ratio [-] | [mm] | Ratio [-] | [mm] | Ratio [-] | |
| ux | 5.000 | 5.000 | 1.000 | 5.018 | 1.004 | 5.000 | 1.000 |
| uz | 20.001 | 20.001 | 1.000 | 20.002 | 1.000 | 20.002 | 1.000 |
| uz | 20.617 | 20.616 | 1.000 | 20.622 | 1.000 | 20.617 | 1.000 |
| Quantity | Analytical Solution | RFEM 5 (Plate-Member) | RFEM 5 (Solid-Member) | RFEM 5 (Solid-Plate) | |||
| [mm] | [mm] | Ratio [-] | [mm] | Ratio [-] | [mm] | Ratio [-] | |
| ux | 5.000 | 5.000 | 1.000 | 5.018 | 1.004 | 5.000 | 1.000 |
| uz | 20.001 | 20.001 | 1.000 | 20.002 | 1.000 | 20.002 | 1.000 |
| uz | 20.617 | 20.617 | 1.000 | 20.621 | 1.000 | 20.617 | 1.000 |