engineAnalysisType Complex Type |
engineAnalysisType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
![]() | ||
![]() | [0, 1] | Bypass ratio at takeoff |
![]() | [0, 1] | Fan pressure ratio at takeoff |
![]() | [0, 1] | DryMass of engine |
![]() | [0, 1] | Design tip relative mach number (FAN) |
![]() | [0, 1] | Maximum rotations per second, shaft 1 |
![]() | [0, 1] | Maximum rotations per second, shaft 2 |
![]() | [0, 1] | overall pressure ratio at takeoff |
![]() | [0, 1] | enginePerformanceMapsType |
![]() | [0, 1] | Thrust at takeoff |
Name | Type | Required | Description |
---|---|---|---|
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