enginePerformanceMapType Complex Type |
enginePerformanceMapType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
All | ||
bleedAirOfftake | doubleBaseType | |
description | [0, 1] | stringBaseType |
eiCO | [0, 1] | Emission index Carbon Monoxide |
eiHC | [0, 1] | Emission index unburned hydrocarbon |
eiNOx | [0, 1] | Emission index Nitrogen Oxide |
eiSoot | [0, 1] | Emission index Soot |
eiSOx | [0, 1] | Emission index Sulfur Oxide |
etaPFan | [0, 1] | Fan efficiency |
flightLevel | [0, 1] | Flight Level |
machNumber | [0, 1] | Mach number |
mDot18 | [0, 1] | Mass flow through bypass nozzle |
mDot8 | [0, 1] | Mass flow through core engine nozzle |
mDotFuel | [0, 1] | Fuel mass flow |
n1 | [0, 1] | Percent of n1Max, shaft 1 |
n2 | [0, 1] | Percent of n2Max, shaft 2 |
name | stringBaseType | |
nozzA18 | [0, 1] | area at bypass outlet |
nozzA8 | [0, 1] | area at core outlet |
piFan | [0, 1] | Fan pressure ratio |
powerOfftake | doubleBaseType | |
rho18 | [0, 1] | air density at bypass outlet 18 |
rho8 | [0, 1] | air density at core outlet 8 |
t18 | [0, 1] | Total temperature at bypass nozzle |
t8 | [0, 1] | Total temperature at core engine nozzle |
tET | [0, 1] | Turbine entry total temperature |
thrust | [0, 1] | Absolute thrust [N] |
v18 | [0, 1] | Speed at bypass nozzle |
v8 | [0, 1] | Speed at core engine nozzle |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string | ||
uID | ID | Yes |