| segment Element |
The aerodynamic coefficients of a fuselage segment
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 Sequence | ||
 segmentUID | Reference to the fuselage segment | |
| strip | [1, *] | Aerodynamic force- and moment coefficients of a fuselage strip |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
Remarks0. General overview
This type contains the aerodynamic coefficients of one fuselage segment.
1. <segmentUID> (mandatory)
A reference to the fuselage segment.
2. <strip> (mandatory)
A list of nodes, each containing the local aerodynamic coefficients of a fuselage segment's strip.
See Also