After the calculation, parts lists are available in the Parts Lists table category.
This category represents a summary of the members, surfaces, and solids used, sorted by materials. The parts lists include all objects that have identical properties ("items").
The 'All by Material' table provides a general survey of the materials and objects used.
In the 'Total Mass' column, the weight of the individual items is shown. The total mass of the model can be seen in the last row.
Customer Project
Customer Project
Customer Project
Customer Project
Customer Project
The results of solid stresses can be displayed as colored 3D points in the finite elements.
Do you have individual column sections and angled wall geometries, and need punching shear design for them?
No problem. In RFEM 6, you can perform punching shear design not only for rectangular and circular sections, but for any cross-section shape.
For a response spectrum analysis of building models, you can display the sensitivity coefficients for the horizontal directions by story.
These key figures allow you to interpret the sensitivity to stability effects.
The modal relevance factor (MRF) can help you to assess to which extent specific elements participate in a specific mode shape. The calculation is based on the relative elastic deformation energy of each individual member.
The MRF can be used to distinguish between local and global mode shapes. If multiple individual members show significant MRF (for example, > 20%), the instability of the entire structure or a substructure is very likely. On the other hand, if the sum of all MRFs for an eigenmode is around 100%, a local stability phenomenon (for example, buckling of a single bar) can be expected.
Furthermore, the MRF can be used to determine critical loads and equivalent buckling lengths of certain members (for example, for stability design). Mode shapes for which a specific member has small MRF values (for example, < 20%) can be neglected in this context.
The MRF is displayed by mode shape in the result table under Stability Analysis → Results by Members → Effective Lengths and Critical Loads.
