fuselageAeroPerformanceType Complex Type

fuselageAeroPerformanceType

Namespace: Empty

Schema: Empty

Base Type
Usages
Children
NameOccurrencesDescription
Sequence Sequence
      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!)

      Element aeroPerformanceMaps

Calculated aerodynamic performance maps of the fuselage

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
Remarks
fuselageAeroPerformance type, containing perfomance maps with aerodynamic data of a fuselage.