| fuselage Element |
Aerodynamic coefficients of a fuselage
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 coefficients | Data type containing a set of aerodynamic coefficients | |
| fuselageUID | Reference to the fuselage segment | |
| segments | A list of fuselage segments with their coefficients. |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
Remarks0. General overview
This type contains the integral aerodynamic coefficients, as well as spanwise coefficient distributions for one fuselage.
1. <fuselageUID> (mandatory)
Reference to the fuselage
2. <coefficients> (mandatory)
Total force and moment coefficients of a fuselage.
3. <segments> (mandatory)
A list of segments with their spanwise coefficient distributions.
See Also