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Line Results on Shells
Returns results as lines painted on the shell mesh. The considered load-case is that set at the nearest upstream ModelView-component.
Inputs
| Name | ID | Description | Type |
|---|---|---|---|
| Analyzed model | Model | Model with calculated displacements | Model |
| LCase | LCase | Name of load-case for which to retrieve results. By default results from load case of index 0 are retrieved. | Generic Data |
| Layer Position | LayerPos | Position on layer '0' for which stresses/strains shall be calculated. -1 designates the lower, +1 the upper side of the shell. | Number |
| Global Force Directions | ForceDirs | List of global directions of force for which flow lines shall be generated. Get projected to elements in case of curved shell geometry and then renders approximate results. | Vector |
| Global Force Direction Position | ForceDirPos | List of points where force directions are given. The force direction selected for an element is equal to the direction closest to the element center. | Vector |
| List of sources of force flow lines (Lines|Points) | Sources | List of lines that intersect the shell or points close to it that define the source of a force flow line. | Generic Data |
| Segment Length [m] | Seg-L | Approximate length of the segments of the stream lines [m]. A negative value means that only INT(-'Seg-L') segments are drawn. | Number |
| dA [deg] | dA | Approximate maximum angle between the segments of the stream lines [deg]. | Number |
| Theta [deg] | Theta | Angular deviation of displayed lines from flow lines [deg]. | Number |
Outputs
| Name | ID | Description | Type |
|---|---|---|---|
| Analyzed model | Model | Analyzed model | Model |
| Lines | Lines | flow lines resulting from the superposition of load-cases as prescribed in the ModelView-component. | Line |
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