| wing Element |
A selected wing with its transition definition
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 lowerSideTransitionRegions | Definition of the parameters for the transition regions | |
| upperSideTransitionRegions | Definition of the parameters for the transition regions | |
| wingUID | [0, 1] | Reference to a wing; required, if separate transition definitions for each wing are used. If missing, transition definitions are the same for all wings. If used, only the specified wings are calculated |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
Remarks0. General overview
Parameters for calculating the viscous drag of a wing, or (if common parameters shall be used) for all wings.
1. <wingUID> (optional)
This node contains a reference to the wing, for which the viscous drag shall be calculated. If all wings shall be computed with common parameters, this node can be omitted.
2. <upperSideTransitionRegions> (mandatory)
In this subnode, the tansition regions and parameters for this region are specified for the upper side of the wing.
3. <lowerSideTransitionRegions> (mandatory)
In this subnode, the tansition regions and parameters for this region are specified for the lower side of the wing.
See Also