Frequently Asked Questions (FAQ) - Search Term: Fatigue D...

• Incorrect Definition of Supports / Lack of Supports
  This can lead to instabilities, as the structure is not supported in all directions. Therefore, the support conditions must be in equilibrium with the structural system as well as with the external boundary conditions. Statically underdetermined systems can also lead to calculation aborts due to a lack of boundary conditions.
  
  
  
  
• Torsion of Members About Their Own Axes
  If members rotate about their own axes, that is, a member is not supported about its own axis, this can lead to instabilities. This is often caused by the settings of member hinges. Thus, it may happen that the torsional releases are entered at both the start node and the end node. However, you should pay attention to the warning that appears when starting the calculation.
  
  
  
  
• Missing Connection of Members
  In the case of large and complex models in particular, it may quickly happen that some members are not connected to each other, thus they "float in the air." Also, if you forget about crossing members that should intersect with each other, this can lead to instabilities as well. The "Crossing Unconnected Members" model check, which searches for members that cross each other but do not have a common node at the intersection point, provides a solution.
  
  
  
  
• No Common Node
  The nodes seem to be at the same location, but on closer inspection, they deviate slightly from each other. This is often caused by CAD imports, and you can correct it using the model check.
  
  
  
  
• Formation of Hinge Chain
  Too many member end hinges on a node can cause a hinge chain that leads to a calculation abort. For each node, only n‑1 hinges with the same degree of freedom relative to the global coordinate system may be defined, where "n" is the number of connected members. The same applies to line releases.
  
  
  
  

2. Check of Stiffening

3. Numerical Problems

4. Detecting Causes of Instability

• Automatic Model Check with Graphical Result Display
  To obtain the graphical display of the instability cause, the RF-STABILITY add-on module (for RFEM 5) or the Structure Stability add-on (for RFEM 6) can help you. To calculate seemingly unstable structures, you can use the options "Calculate eigenvector for unstable model" option (see Image 09) or "Calculate without loading for instability check by mode shape". An eigenvalue analysis is performed using the structural data so that the instability of the affected structural component is displayed graphically as a result.
  
  
  
  
• Critical Load Problem
  If load cases or load combinations are calculated according to the geometrically linear analysis, and the calculation is only aborted as of the second-order analysis, there is a stability problem (critical load factor less than 1.00). The critical load factor indicates the factor by which the loading must be multiplied in order for the model to become unstable (for example, buckling) under the corresponding load. Consequently: A critical load factor smaller than 1.00 means that the structure is unstable. Only a positive critical load factor greater than 1.00 means that the load due to the predefined axial forces multiplied by this factor leads to the buckling failure of the stable structure. In order to find the "weak point", the following approach is recommended, which requires the RF‑STABILITY (RFEM 5) or the RSBUCK (RSTAB 8) add-on module or the Structure Stability add-on (RFEM 6 / RSTAB 9), see also the video "Critical Load Problem" under "Downloads".
  
  First, it is necessary to reduce the load of the affected load combination until the load combination becomes stable. The load factor in the calculation parameters of the load combination can help. This also corresponds to the manual determination of the critical load factor if the add-on modules or add-ons mentioned above are not available. For purely linear structural elements, it may already be sufficient to calculate the load combination according to the linear static analysis and use it directly in the add-on module, or determine the critical load using the add-on. Using the graphical buckling mode of this load combination, you can possibly find the "problematic location" in the structure and fix the problem. In order to also determine the local mode shapes, it is necessary to activate the member division in the RF‑STABILITY add-on module (RFEM 5), or at least to increase the division for trusses to "2" in the RSBUCK add-on module (RSTAB 8). In the Structure Stability add-on (RFEM 6 / RSTAB 9), you should just check whether the member division has been activated for the members.
  
  
  
  

• Cohesive soil
• Pure silt - UL
• Stiff consistency
• Embedment depth of the foundation t = 4.92 ft