Differences of Calculation Methods in Structural Analysis
Technical Article
For structural dimensioning according to the valid rules, there are often several options or calculation methods to determine the internal forces. It is up to the engineer to decide which theory is suitable to design the structure.
Basically, there are two different calculation methods: the linear static analysis and the secondorder analysis. As a special form of the calculation according to the secondorder analysis, the large deformation analysis is available.
Basics of Analytical Model
As a calculation example, there is a cantilever beam with a length of 3.0 m. The head load is 18 kN in the horizontal direction of the major axis and 30 kN in the vertical direction. The designed crosssection is HEA 180 made of the structural steel S235.
Calculation According to Linear Static Analysis
The calculation of internal forces according to the linear static analysis describes a linear calculation on an undeformed system. It is assumed that no deformations arise. In many cases of the general structural analysis, this approach is sufficient.
The moment at the column base is calculated as follows:
${\mathrm M}_\mathrm I\;=\;\mathrm H\;\cdot\;\mathrm l$
Figure 02  Results of Linear Static Analysis
Calculation According to SecondOrder Analysis
The calculation according to the secondorder analysis describes a nonlinear calculation of the structure on a deformed system. This means that the arising deformations have an influence on the internal forces. The acting axial force additionally increases the moment on the support nodes of the column.
In this case, the moment is:
${\mathrm M}_\mathrm{II}\;=\;\mathrm H\;\cdot\;\mathrm l\;+\;\mathrm N\;\cdot\;{\mathrm e}_\mathrm X$
Figure 03  Results of SecondOrder Analysis
However, this analysis method assumes small deformations, since it only considers deformations, but no rotation of the structure. In the computational calculation, the linear analysis is used to determine the axial forces of the member, and in the second iteration, the additional moment is calculated from the deformation. The iteration diagram of RFEM reflects this behaviour.
Figure 04  Iteration Diagram of SecondOrder Analysis
The modification of the internal forces N and V with respect to the deformation is not further considered according to this calculation method. In RFEM, however, it is possible to convert the internal forces of the secondorder analysis to the deformed structure, and thus perform the design.
Calculation According to Large Deformation Analysis
This calculation method also takes into account the rotation of the structure. It is a nonlinear calculation, like the secondorder analysis. After each iteration step, the stiffness matrix of the deformed system is generated and the calculation continues until the equilibrium is reached.
Figure 05  Results of Large Deformation Analysis
Figure 06  Iteration Diagram of Large Deformation Analysis
The resulting moment at the column base is as follows:
${\mathrm M}_\mathrm{III}\;=\;\mathrm H\;\cdot\;(\mathrm l\;\;{\mathrm e}_\mathrm Z)\;+\;\mathrm N\;\cdot\;{\mathrm e}_\mathrm X$
Figure 07  Head Deformation eX, eZ
The comparison of the member internal forces shows that the calculation according to the large deformation analysis has also an influence on the shear and axial forces of the structure.
Summary
The results of the different calculation methods show that the deformation does have an impact on the internal forces. In this case, the calculation according to the large deformation analysis seems to be the most accurate, but it also takes the most computing time. Moreover, some effects (torsional forces, etc.) may arise in the case of the large deformation analysis, causing difficulties in further design. Therefore, it is necessary to exactly check which calculation method is required for the given structure. In this case, you can follow the rule to perform the calculation 'as simple as possible, but as accurate as necessary'.
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Figure 01  Structural System

Figure 02  Results of Linear Static Analysis

Figure 03  Results of SecondOrder Analysis

Figure 04  Iteration Diagram of SecondOrder Analysis

Figure 05  Results of Large Deformation Analysis

Figure 06  Iteration Diagram of Large Deformation Analysis

Figure 07  Head Deformation eX, eZ