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coefficientsBreakdownSegmentType Complex Type

Aerodynamic contributions of a wing segment

Namespace: Empty

Schema: Empty

Base Type
Usages
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.