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coefficientsBreakdownWingType Complex Type

Aerodynamic contributions of a wing

Namespace: Empty

Schema: Empty

Base Type
Usages
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.