Lightweight Timber Structure
Model to Download
Model of the master thesis "Comparison with Respect to Load-Bearing Capacity of Two Structural Systems of Walls with Straw Bales Carried out 'in situ': Column System and Modified CUT System," associated with the results of the wall stiffness of the module built with the modified Cut structural system.
The stresses in the cross‑section of the member are calculated in the so‑called stress points. These points are set at such locations in the cross‑section, at which the extreme values for the stresses due to the loading types can occur in the material.
Model of the Final Master's Thesis "Comparative, with respect to the bracing capacity of two construction systems of straw bale walls made" in situ "
The cross-section resistance design analyzes tension and compression along the grain, bending, bending and tension/compression as well as the strength in shear due to shear force.
The design of structural components at risk of buckling or lateral-torsional buckling is performed according to the Equivalent Member Method and considers the systematic axial compression, bending with and without compressive force as well as bending and tension. Deflection of inner spans and cantilevers is compared to the maximal allowable deflection.
Separate design cases allow for a flexible and stability analysis of members, sets of members, and loads.
Design-relevant parameters such as the stability analysis type, member slendernesses, and limit deflections can be freely adjusted.
- Where do I find the setting to specify the entered structural component as a "wall" or "slab"?
- Is it possible to set user-defined values when viewing solid stress results?
- Is it possible to display more values for the stress distribution over the layers in RF‑LAMINATE?
- Which add-on modules and programs do I need for laminate and sandwich structures as well as cross-laminated timber (CLT)?
- Can I quickly optimize all cross-sections in my model by using internal forces?
- How can I control an overpressed joint in the ridge?
- "During the calculation of material non-linearity, the material with a decreasing branch of the diagram can be calculated with one load increment only." Why do I get this error?
- How do I display some results of all load cases in the printout report, but other results of the selected load cases only?
- How does the "Orthotropic Plastic" material model work in RFEM?
- The calculation of my model results in unrealistically high stresses at many locations. What is the reason?