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Load case
|
Load case to be added to the RmSet (s. examples) |
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Result for given envelope/envelope row
|
Result of previously specified envelope(s) (s. above) to be added to the RmSet (s. examples) |
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Load case result
|
Result of one load case to be added to the RmSet (s. examples) |
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Schedule
|
Schedule name (may be left blank) |
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Load case name
|
Name of the load case results wanted to be output | Setting | Description |
|---|
| 1st selection arrow |
List of all user defined load cases (input load cases) |
| 2nd selection arrow |
List of all user defined and internally generated load cases (result load cases) |
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Result component
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Result component to be output: Vx, ..., Mz . | Setting | Description |
|---|
| Stress |
Stress for the specified stress point |
| TAUY, TAUZ |
Shear stresses |
| SIGI,SIGII, SIGIII |
Principal stresses acc. to chosen mode (s. 'General') |
| Reinforcement stress |
for the specified attribute set |
| Tendon stress |
for the specified tendon |
| Elastic strain |
The function allows for presenting the longitudinal strain in the different stress points in the cross-section.
Note: The presented strain value is only the linearly elastic part of the total strain, i.e. the value recalculated from element forces by using the E-Modulus.
The values do not contain temperature strains, viscous strains due to creep and shrinkage and any non-linear strain parts due to material non-linearity.
|
| All internal forces |
6 rows for all internal forces will be added A row with key 'Nx-Mz' will be inserted in the list
When the RmSet is saved this row has been splitted into 6 rows (1 per force)
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|
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Schedule
|
Schedule name (can be left blank) |
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Load case name
|
Name of the load case results wanted to be output |
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Stress point
|
Stress point the stress wanted to be output for |
|
Attribute set
|
Attribute set the reinforcement stress wanted to be output for |
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Tendon number
|
Tendon the tendon stress wanted to be output for |
