| wing Element |
Aerodynamic contributions of a wing
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 Sequence | ||
 wingUID | Reference to a wing uID | |
| coefficients | Aerodynamic coefficients | |
| Sequence | [0, 1] | |
| segments | Aerodynamic contributions of wing segments | |
| remainingContributions | [0, 1] | Remaining contributions to aerodynamic coefficients |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
RemarksDescribes the contributions of a specific wing to the total aerodynamic coefficients of a vehicle
It is obligatory to reference a wing via its uID and to provide its coefficients. The breakdown of the coefficients comprises the segments and remainingContributions. The latter must only be specified if segments is given.
See Also