coefficientsBreakdownWingType Complex Type |
Aerodynamic contributions of a wing
Namespace: Empty
Schema: Empty
Base Type
UsagesChildren| 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.