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fuselageAeroPerformanceType Complex Type

Fuselage aerodynamic performance

Namespace: Empty

Schema: Empty

Base Type
Usages
Children
NameOccurrencesDescription
All All
      Element aeroPerformanceMaps

Calculated aerodynamic performance maps

      Element fuselageUID

Reference to the UID of the analysed fuselage

      Element reference[0, 1]

References used for the calculation of the force and moment coefficients of the fuselage (in the fuselage axis system!)

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string

Directory of the external data file

Attribute externalDataNodePathSimple Type string

Path of the node inside the external data file

Attribute externalFileNameSimple Type string

Name of the external data file

Remarks
Performance maps with aerodynamic data of a fuselage.