| engineGeometryType Complex Type |
Definition of the global engine geometry.
Namespace: Empty
Schema: Empty
Base Type
UsagesChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 chordlength | [0, 1] | Chordlength of a fan blade |
| diameter | [0, 1] | Diameter |
| diameterProp | [0, 1] | dProp |
| engineMounts | [0, 1] | Mounts attaching the engine to the aircraft |
| fan | [0, 1] | Fan |
| length | [0, 1] | Length |
| liner | [0, 1] | Acoustic liner |
| spinner | [0, 1] | Spinner |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | Directory of the external data file | |
| externalDataNodePath | string | Path of the node inside the external data file | |
| externalFileName | string | Name of the external data file |
RemarksAll engine geometry definitions refer to the engine coordinate system. The engine coordinate system has its orgine in the middle of the fan plan. The positive x-axis is heading to the rear, the positive z-axis to the top and the y-axis according to the right hand rule.