segment Element

Aerodynamic contributions of a wing segment

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Sequence Sequence
      Element segmentUID

Reference to a wing segment uID

      Element coefficients

Aerodynamic coefficients

      Sequence Sequence[0, 1]
            Element strips

Aerodynamic contributions of strips within a wing segment

            Element remainingContributions[0, 1]

Remaining contributions to aerodynamic coefficients

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
Remarks

Describes the contributions of a specific wing segment to the total aerodynamic coefficients of a wing

It is obligatory to reference a segment via its uID and to provide its coefficients. The breakdown of the coefficients comprises the strips and remainingContributions. The latter must only be specified if strips is given.

See Also