| wing Element |
Aerodynamic coefficients of a wing
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 coefficients | Data type containing a set of aerodynamic coefficients | |
| segments | A list of wing segments with their coefficients. | |
| wingUID | Reference to the wing segment |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
Remarks0. General overview
This type contains the integral aerodynamic coefficients, as well as spanwise coefficient distributions for one wing.
1. <wingUID> (mandatory)
Reference to the wing
2. <coefficients> (mandatory)
Total force and moment coefficients of a wing.
3. <segments> (mandatory)
A list of segments with their spanwise coefficient distributions.
See Also