| segments Element |
A list of fuselage segments with their coefficients.
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 Sequence | ||
 segment | [1, *] | The aerodynamic coefficients of a fuselage segment |
| calibration | [0, 1] | Data type containing a set of aerodynamic coefficients |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
Remarks0. General overview
This type contains one subnode with aerodynamic coefficients for each of the fuselage's segments.
1. <segment> (mandatory)
A node with the coefficient distributions on one fuselage.
See Also