| methodDLR1 Element |
Method "DLR1 for calculating viscous drag
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 wings | [0, 1] | A list of wings for computation |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
Remarks0. General overview
Calculation of viscous drag by using a flat plate analogy to compute skin friction drag, combined with form factors for additional pressure drag due to viscous separation. The flat plate is computed including laminar-turbulent transition, with the transition position as polynomial function of the local Reynolds number.
1. <wings> (optional)
This node contains a list of wings and theit parameters for computation with this method.
See Also