Select the result component for the result presentation of design checks for 3D-diagrams
Select the result name, for which you want to display the results, in the Result Data under Design Checks.
Depending on the selected result name (of a certain design check) and on the type of the property set, respective result components are available, which are listed in the following.
Use the right button in this task area to create a three-dimensional interaction diagram for the check in the ULS (select the respective file (*.stl) from the subfolder for the results of the checks in the ULS).
Results from the design in the ULS: Longitudinal reinforcement (bending + normal force, shear force, torsion, crack)
ASuser
Amount of reinforcement defined by the user
Note: Input the user-defined reinforcement area within the respective property set in the cross section definition.
ASd
Evaluated amount of reinforcement due to the design in the ULS
Note: The amount of the user-defined reinforcement is not included.
ASmax
Greater value from ASuser and ASd
Note: That means, that either the user-defined or the evaluated amount of reinforcement is decisive.
ASuser <= ASd -> ASmax = ASd
ASuser > ASd -> ASmax = ASuser
Results from the design in the ULS: Stirrup reinforcement (shear and torsion)
Asw, Aswd, Aswmax
Stirrup reinforcement; for details see (analogously) above
Results from the check due to bending
Utilization
Utilization ratio; ratio of the acting design bending moment to the design bending moment of resistance
MEd
Resultant vector of the acting design bending moment
MEdy
Design value of the acting bending moment about the y-axis
MEdz
Design value of the acting bending moment about the z-axis
MRd1
(First) design value of the bending moment of resistance, calculated for NEd = const. (value closer to MEd in the interaction diagram)
MRd2
(Second) design value of the bending moment of resistance, calculated for NEd = const. (value farther from MEd in the interaction diagram)
NEd
Design value of the acting normal force
Results from the check due to shear
Utilization
Utilization ratio; ratio of the acting design shear force to the design shear force of resistance
Results from the check due to torsion
Utilization
Utilization ratio; ratio of the acting design torsional moment to the design torsional moment of resistance
Results from the check due to interaction of shear + torsion
Utilization
Utilization ratio; ratio of the acting design shear force to the design shear force of resistance
Results from the stress checks
Uconc
Utilization ratio of the concrete in regard to the maximum calculated stress; ratio of the maximum calculated stress to the allowable stress
Ureinf
Utilization ratio of the reinforcing steel in regard to the maximum calculated tensile stress; ratio of the maximum calculated tensile stress to the allowable tensile stress
Utend
Utilization ratio of the prestressing steel in regard to the maximum calculated stress; ratio of the maximum calculated tensile stress to the allowable tensile stress
Utilization
Greatest value from Uconc, Ureinf und Utend
sc,max
Maximum compression stress in the concrete
ss,max
Maximum tensile stress in the reinforcing steel
sp,max
Maximum tensile stress in the prestressing steel
Results from the check for the limitation of the crack width
Ucw
Utilization ratio of the crack width; ratio of the calculated crack width to the allowable crack width
Utilization
Greatest value from Ucw and Udc
Wk
Greatest evaluated crack width
Udc
Utilization ratio of decompression; ration of the calculated decompression height (distance from the neutral axis) to the allowable decompression height
DcDistance
Calculated decompression height of the tendons from the neutral axis
Results from the calculation of the linear normal stresses and principal stresses
Sigma x, max
Calculated maximum normal stress (tensile stress) from all vertices of the cross section and all user-defined stress points
Sigma x, min
Calculated minimum normal stress (compression stress) from all vertices of the cross section and all user-defined stress points
Sigma 1
Calculated maximum principal stress (tensile stress) from all vertices of the cross section and all user-defined stress points
Sigma 2
Calculated minimum principal stress (compression stress) from all vertices of the cross section and all user-defined stress points
Results from the fatigue check
Utilization
Utilization ratio related to the damage
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