fuselage Element |
Aerodynamic coefficients of a fuselage
Namespace: Empty
Schema: Empty
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. |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |
This type contains the integral aerodynamic coefficients, as well as spanwise coefficient distributions for one fuselage.
Reference to the fuselage
Total force and moment coefficients of a fuselage.
A list of segments with their spanwise coefficient distributions.