| fuselage Element |
Fuselage
Namespace: Empty
Schema: Empty
| Name | Occurrences | Description |
|---|---|---|
| | [0, 1] | Compartments |
| | [0, 1] | Cut-outs |
| | [0, 1] | Decks |
| | [0, 1] | Description |
| | [0, 1] | Fuel tanks |
| | Name | |
| | [0, 1] | UID of part to which the fuselage is mounted (if any) |
| | [0, 1] | Positionings of the fuselage sections |
| | Sections | |
| | Segments | |
| | [0, 1] | Structural layout |
| | Position and orientation |
| Name | Type | Required | Description |
|---|---|---|---|
Directory of the external data file | |||
Path of the node inside the external data file | |||
Name of the external data file | |||
Continuity used for lofting this component (default: C2 for fuselages and ducts, C0 for wings) | |||
Symmetry plane the component is mirrored at | |||
| Yes | UID |