analysis Element |
engineAnalysisType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
thrust00 | [0, 1] | Thrust at takeoff |
fpr00 | [0, 1] | Fan pressure ratio at takeoff |
bpr00 | [0, 1] | Bypass ratio at takeoff |
opr00 | [0, 1] | overall pressure ratio at takeoff |
n1Max | [0, 1] | Maximum rotations per second, shaft 1 |
n2Max | [0, 1] | Maximum rotations per second, shaft 2 |
mTrD | [0, 1] | Design tip relative mach number (FAN) |
mass | [0, 1] | DryMass of engine |
performanceMaps | [0, 1] | enginePerformanceMapsType |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |