reference Element |
Reference values for local aerodynamic coefficients.
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
All | ||
area | doubleBaseType | |
flightShapePoint | pointXYZType | |
jigShapePoint | pointXYZType | |
length | doubleBaseType |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |
This type contains the reference values used for normalizing local aerodynamic coefficients. The reference point is defined in absolut CPACS-coordinates.
Flight shape point, specified in absolut CPACS-coordinates The reference point is used as origin for calculating the local moment coefficients. See the documentation of the global CPACS-Element for further information.
Jig shape point, specified in absolut CPACS-coordinates. The corredponding point on the initial CPACS geometry.
Local reference area.
Local reference length, used for normalizing all the moment coefficients. The length is always given in the middle of the wing segment.