performanceMap Element |
enginePerformanceMapType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
![]() | ||
![]() | doubleBaseType | |
![]() | [0, 1] | stringBaseType |
![]() | [0, 1] | Emission index Carbon Monoxide |
![]() | [0, 1] | Emission index unburned hydrocarbon |
![]() | [0, 1] | Emission index Nitrogen Oxide |
![]() | [0, 1] | Emission index Soot |
![]() | [0, 1] | Emission index Sulfur Oxide |
![]() | [0, 1] | Fan efficiency |
![]() | [0, 1] | Flight Level |
![]() | [0, 1] | Mach number |
![]() | [0, 1] | Mass flow through bypass nozzle |
![]() | [0, 1] | Mass flow through core engine nozzle |
![]() | [0, 1] | Fuel mass flow |
![]() | [0, 1] | Percent of n1Max, shaft 1 |
![]() | [0, 1] | Percent of n2Max, shaft 2 |
![]() | stringBaseType | |
![]() | [0, 1] | area at bypass outlet |
![]() | [0, 1] | area at core outlet |
![]() | [0, 1] | Fan pressure ratio |
![]() | doubleBaseType | |
![]() | [0, 1] | air density at bypass outlet 18 |
![]() | [0, 1] | air density at core outlet 8 |
![]() | [0, 1] | Total temperature at bypass nozzle |
![]() | [0, 1] | Total temperature at core engine nozzle |
![]() | [0, 1] | Turbine entry total temperature |
![]() | [0, 1] | Absolute thrust [N] |
![]() | [0, 1] | Speed at bypass nozzle |
![]() | [0, 1] | Speed at core engine nozzle |
Name | Type | Required | Description |
---|---|---|---|
![]() | ![]() | ||
![]() | ![]() | ||
![]() | ![]() | ||
![]() | ![]() | Yes |