| controlSurfaceHingeMomentMapType Complex Type |
Control surface hinge moment map
Namespace: Empty
Schema: Empty
Base Type
UsagesChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 controlParameters | Control parameters | |
| controlSurfaceUID | Reference to the control surface | |
| dcd | [0, 1] | Increment of the drag coefficient due to the control surface deflection |
| dcl | [0, 1] | Increment of the lift coefficient due to the control surface deflection |
| dcmd | [0, 1] | Increment of the moment coefficient around the d-axis due to the control surface deflection |
| dcml | [0, 1] | Increment of the moment coefficient around the l-axis due to the control surface deflection |
| dcms | [0, 1] | Increment of the moment coefficient around the s-axis due to the control surface deflection |
| dcs | [0, 1] | Increment of the side force coefficient due to the control surface deflection |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | Directory of the external data file | |
| externalDataNodePath | string | Path of the node inside the external data file | |
| externalFileName | string | Name of the external data file |
RemarksMoment map with aerodynamic data for a control surface. Array order is: controlParameters min->max then angleOfAttack then angleOfSideslip then reynoldsNumber then machNumber. AngleOfAttack, angleOfSideslip, reynoldsNumber and machNumber are taken from the basic performance map one level above.