segment Element |
The aerodynamic coefficients of a fuselage segment
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
segmentUID | Reference to the fuselage segment | |
strip | [1, *] | Aerodynamic force- and moment coefficients of a fuselage strip |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |
This type contains the aerodynamic coefficients of one fuselage segment.
A reference to the fuselage segment.
A list of nodes, each containing the local aerodynamic coefficients of a fuselage segment's strip.