coefficientsBreakdownType Complex Type |
Aerodynamic coefficients breakdown
Namespace: Empty
Schema: Empty
Base Type
UsagesChildren| Name | Occurrences | Description |
|---|---|---|
 Choice | ||
 Sequence | ||
 wings | Aerodynamic contributions of the wings | |
| otherComponents | [0, 1] | Aerodynamic contributions of the components |
| remainingContributions | [0, 1] | Remaining contributions to aerodynamic coefficients |
| Sequence | ||
| otherComponents | Aerodynamic contributions of the components | |
| remainingContributions | [0, 1] | Remaining contributions to aerodynamic coefficients |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
RemarksBreakdown of the total aerodynamic coefficients into contributions from the various vehicle componenents. A detailed breakdown is only specified for the wing. Other components, such as the fuselage, are more generically referred to as otherComponents. Since the sum of the contributions within a breakdown must equal the total coefficients, the remaining contributions must be listed in remainingContributions.
The remainingContributions cannot be defined alone. Either the definition of a wing, otherComponents or both together is valid and can be combined with remainingContributions.