loadCase Element |
A loadcase for computation with HandbookAero
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
All | ||
description | [0, 1] | Description of the loadcase |
flow | This type contains a complete set of flow condition data | |
loadCaseUID | Reference to a loadcase | |
name | Name of the loadcase | |
totalCoefficients | [0, 1] | Data type containing a set of aerodynamic coefficients |
wings | [0, 1] | List of wing coefficient nodes for each wing |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |
This type contains the whole set of operational parameters, required to compute a single loadcase with HandbookAero.
This is the name of the loadcase.
This is the the description of the loadcase.
This is a reference to the original loadcase definition within the selected aircraft model. It is used to locate the place, where the tool results have to be stored.
This node contains the definition of the flow conditions for the aerodynamic computations.
If HandbookAero is used to extend / modify existing loadcase data, this node has to contain the total coefficients for the specific loadcase.
If HandbookAero is used to extend / modify existing loadcase data, this node has to contain the aerodynamic coefficients for all the wings.