| intermediateAirfoil Element |
Airfoil contour between the inner and the outer border
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 airfoilUID | Reference to the airfoil UID | |
| eta | Relative spanwise coordinate (eta) of the control surface, where the leading edge of the airfoil is placed | |
| rotX | Rotation around an axis, going from the leading edge point to the trailing edge point of the control surface. Defaults to 90°, which is equivalent to perpendicular on the control surface middle plane. | |
| rotZ | Rotation of the airfoil around the control surface middle plane normal direciotn. Reference point is the most forward point of the airfoil. Defaults to 90°, which is equivalent to the airfoilplacement in flight direction (along wings-x axis). | |
| scalY | Scaling of the airfoil in spanwise direction (not used for 2D airfoils) | |
| scalZ | Scaling in thickness direction of the airfoil |
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 |
See Also