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analysis Element

engineAnalysisType

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
All All
      Element bpr00[0, 1]

Bypass ratio at takeoff

      Element fpr00[0, 1]

Fan pressure ratio at takeoff

      Element mass[0, 1]

DryMass of engine

      Element mTrD[0, 1]

Design tip relative mach number (FAN)

      Element n1Max[0, 1]

Maximum rotations per second, shaft 1

      Element n2Max[0, 1]

Maximum rotations per second, shaft 2

      Element opr00[0, 1]

overall pressure ratio at takeoff

      Element performanceMaps[0, 1]

enginePerformanceMapsType

      Element thrust00[0, 1]

Thrust at takeoff

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
See Also

Reference

engineType