| fuselages Element |
List of fuselage coefficient nodes for each wing
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 Sequence | ||
 fuselage | [1, *] | Aerodynamic coefficients of a fuselage |
| 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 coefficients for each of the fuselages.
1. <fuselage> (mandatory)
Aerodynamic coefficients for a single fuselage.
2. <calibration> (optional)
Aerodynamic coefficients for additional entities used for calibration.
See Also