Online manuals, introductory examples, tutorials, and other documentation.
3.3.2 Nonlinear Method
Performing a design according to the Nonlinear method requires a license of the add-on module RF-CONCRETE NL. This method for the serviceability limit state design is described in detail in chapter 2.8.
The following columns are described in the previous chapter 3.3.1:
- wk,-z(top) / wk,+z(bottom)
For orthotropic surfaces, a serviceability limit state design according to the nonlinear method is not possible.
The values in the columns D through J are controlled in the tabs below. The settings specified in them are applied to all surfaces by default. It is also possible to assign the current settings only to certain surfaces: Clear the selection of the All check box. Then, enter the numbers of the relevant surfaces or use the button to select them graphically. With you assign the current settings to these surfaces.
The assignment is only applicable for the active tab, for example Stress Check.
The parameters for creep must be defined in the Creeping tab (see Figure 2.144). Based on these conditions, the program determines the creep coefficient φ. For the effective structural component thickness h0, the program applies the surface thickness d.
The determination of the creep coefficient is described in chapter 18.104.22.168.
This column shows the shrinkage strain. The relevant parameters must be defined in the Shrinkage tab (see Figure 2.147). Based on these conditions, the program determines the shrinkage strain εcs. For the effective structural component thickness h0, the program applies the surface thickness d.
The determination of the shrinkage strain is described in chapter 22.214.171.124. If you do not wish to apply any shrinkage strain to a surface, you must set the user-defined shrinkage strain to zero in the Shrinkage tab, and then apply it to the surface.
For pure plates that are defined as model type 2D - XY (uZ/φX/φY), it is not possible to consider shrinkage: There are only degrees of freedom for bending.
This value represents the maximum allowable deformation that must be observed in the design of the serviceability limit state. The design criteria are defined in the Deformation Analysis tab.
The serviceability for "common structures", for example according to EN 1992-1-1, clause 7.4, is ensured if the deflection in the quasi-permanent action combination does not exceed the following limit values.
Structural elements for which excessive deformations can result in subsequent damages:
The Minimum boundary line, Maximum boundary line, and User-defined relative options determine which effective length leff will be applied. For the two boundary line options, the program applies the shortest and the greatest border line of the respective surface.
When you choose the User-defined relative option, you can enter the length directly or select it graphically between any two points in the RFEM model with . Furthermore, for all three options you must define a divisor by which the lengths will be divided.
It is also possible to define the allowable maximum deformation uz,max as User-defined absolute.
The deformation design criterion uses the deflection of a surface – the vertical deformation relative to the straight line connecting the points of support. The Deformation Analysis tab (see Figure 3.20) provides three options for how to calculate the local deformation uz,local applied in the design.
The deformation is related to the initial structure.
Displaced parallel surface:
This option is recommended for an elastic support of the surface. The deformation uz,local is related to a virtual reference surface that is displaced parallel to the undeformed system. The displacement vector of the reference surface is as long as the minimal nodal deformation within the surface.
Deformed user-defined reference plane:
If the support deformations of a surface differ considerably from each other in size and degree, you can define an inclined reference plane for the deformation to be checked uz,local. This plane must be defined by three points of the undeformed system. The program determines the deformation of the three definition points, places the reference plane in these displaced points, and then calculates the local deformation uz,local.