segment Element |
Aerodynamic contributions of a wing segment
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 Sequence | ||
 segmentUID | Reference to a wing segment uID | |
| coefficients | Aerodynamic coefficients | |
| Sequence | [0, 1] | |
| strips | Aerodynamic contributions of strips within a wing segment | |
| 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 segment to the total aerodynamic coefficients of a wing
It is obligatory to reference a segment via its uID and to provide its coefficients. The breakdown of the coefficients comprises the strips and remainingContributions. The latter must only be specified if strips is given.
See Also