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coefficientsBreakdown Element

Aerodynamic coefficients breakdown

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Choice Choice
      Sequence Sequence
            Element wings

Aerodynamic contributions of the wings

            Element otherComponents[0, 1]

Aerodynamic contributions of the components

            Element remainingContributions[0, 1]

Remaining contributions to aerodynamic coefficients

      Sequence Sequence
            Element otherComponents

Aerodynamic contributions of the components

            Element remainingContributions[0, 1]

Remaining contributions to aerodynamic coefficients

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

Breakdown of the total aerodynamic coefficients into contributions from the various vehicle componenents. A detailed breakdown is only specified for the wing. Other components, such as the fuselage, are more generically referred to as otherComponents. Since the sum of the contributions within a breakdown must equal the total coefficients, the remaining contributions must be listed in remainingContributions.

The remainingContributions cannot be defined alone. Either the definition of a wing, otherComponents or both together is valid and can be combined with remainingContributions.

See Also