wing Element

Aerodynamic contributions of a wing

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Sequence Sequence
      Element wingUID

Reference to a wing uID

      Element coefficients

Aerodynamic coefficients

      Sequence Sequence[0, 1]
            Element segments

Aerodynamic contributions of wing segments

            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 to the total aerodynamic coefficients of a vehicle

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

See Also