outputOptions Element

Output options for this wing.

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
All All
      Element destinationWingUID

Destination UID of the wing which will be written into the CPACS file.

      Element numberOfPointsPerSection[0, 1]

Number of points per section. If not specified, the value specified in the global output options is used.

      Element numberOfSections[0, 1]

Number of sections. If not specified, the value specified in the global output options is used.

      Element parentUID[0, 1]

UID of part to which the wing is mounted (if any). The parent of the wing can e.g. be the fuselage. In each aircraft model, there is exactly one part without a parent part (The root of the connection hierarchy).

      Element sectionDistributionMode[0, 1]

Section distribution mode. If not specified, the value specified in the global output options is used.

      Element symmetry[0, 1]

If there exists a mirrored counterpart of the wing: specify the symmetry plane here

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
See Also