delis Element |
delisToolspecificType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
tool | Tool identification | |
aircraftModelUID | UID of the aircraft model | |
lumpMassBreakdownOutput | Flag if the massbreakdown should be written with every single structural item or if the mass sum of each type of structural element of one component should be written. E.g. write all sparCells or write only the sum of the sparCells of the wing. Defaults to false | |
coupleFuselageBT | Flag if coupling with the BT fuselage should be performed. In this case, DELiS creates only wings and the ansys components for coupling with Trafuma. If False, also a DELiS fuselage will be created, if given and requested and coupled with the DELiS wings. Defaults to false | |
useAeroCoefficientAndNodalInertialLoads | Flag if the loadcase AeroCoefficientAndNodalInertialLoadsLoadCase should be used before other loadcases Defaults to False | |
createdComponents | [0, 1] | Optional list of ComponentIDs of the component(wing or fuselage) that should be modeled. If not set all components are modeled. |
wings | [0, 1] | List of wings to set specific model and sizing settings. If not specified, default values are used. |
fuselages | [0, 1] | List of fuselages to set specific model and sizing settings. If not specified, default values are used. |
sizingConvergence | [0, 1] | delisSizingConvergenceType |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |